'''
MAVLink protocol implementation (auto-generated by mavgen.py)

Generated from: common.xml

Note: this file has been auto-generated. DO NOT EDIT
'''

import struct, array, time, json, os, sys, platform

from ...generator.mavcrc import x25crc

WIRE_PROTOCOL_VERSION = "1.0"
DIALECT = "mavlink"

native_supported = platform.system() != 'Windows' # Not yet supported on other dialects
native_force = 'MAVNATIVE_FORCE' in os.environ # Will force use of native code regardless of what client app wants
native_testing = 'MAVNATIVE_TESTING' in os.environ # Will force both native and legacy code to be used and their results compared

if native_supported:
    try:
        import mavnative
    except ImportError:
        print("ERROR LOADING MAVNATIVE - falling back to python implementation")
        native_supported = False

# some base types from mavlink_types.h
MAVLINK_TYPE_CHAR     = 0
MAVLINK_TYPE_UINT8_T  = 1
MAVLINK_TYPE_INT8_T   = 2
MAVLINK_TYPE_UINT16_T = 3
MAVLINK_TYPE_INT16_T  = 4
MAVLINK_TYPE_UINT32_T = 5
MAVLINK_TYPE_INT32_T  = 6
MAVLINK_TYPE_UINT64_T = 7
MAVLINK_TYPE_INT64_T  = 8
MAVLINK_TYPE_FLOAT    = 9
MAVLINK_TYPE_DOUBLE   = 10


class MAVLink_header(object):
    '''MAVLink message header'''
    def __init__(self, msgId, mlen=0, seq=0, srcSystem=0, srcComponent=0):
        self.mlen = mlen
        self.seq = seq
        self.srcSystem = srcSystem
        self.srcComponent = srcComponent
        self.msgId = msgId

    def pack(self):
        return struct.pack('BBBBBB', 254, self.mlen, self.seq,
                          self.srcSystem, self.srcComponent, self.msgId)

class MAVLink_message(object):
    '''base MAVLink message class'''
    def __init__(self, msgId, name):
        self._header     = MAVLink_header(msgId)
        self._payload    = None
        self._msgbuf     = None
        self._crc        = None
        self._fieldnames = []
        self._type       = name

    def get_msgbuf(self):
        if isinstance(self._msgbuf, bytearray):
            return self._msgbuf
        return bytearray(self._msgbuf)

    def get_header(self):
        return self._header

    def get_payload(self):
        return self._payload

    def get_crc(self):
        return self._crc

    def get_fieldnames(self):
        return self._fieldnames

    def get_type(self):
        return self._type

    def get_msgId(self):
        return self._header.msgId

    def get_srcSystem(self):
        return self._header.srcSystem

    def get_srcComponent(self):
        return self._header.srcComponent

    def get_seq(self):
        return self._header.seq

    def __str__(self):
        ret = '%s {' % self._type
        for a in self._fieldnames:
            v = getattr(self, a)
            ret += '%s : %s, ' % (a, v)
        ret = ret[0:-2] + '}'
        return ret

    def __ne__(self, other):
        return not self.__eq__(other)

    def __eq__(self, other):
        if other == None:
            return False

        if self.get_type() != other.get_type():
            return False

        # We do not compare CRC because native code doesn't provide it
        #if self.get_crc() != other.get_crc():
        #    return False

        if self.get_seq() != other.get_seq():
            return False

        if self.get_srcSystem() != other.get_srcSystem():
            return False            

        if self.get_srcComponent() != other.get_srcComponent():
            return False   
            
        for a in self._fieldnames:
            if getattr(self, a) != getattr(other, a):
                return False

        return True

    def to_dict(self):
        d = dict({})
        d['mavpackettype'] = self._type
        for a in self._fieldnames:
          d[a] = getattr(self, a)
        return d

    def to_json(self):
        return json.dumps(self.to_dict())

    def pack(self, mav, crc_extra, payload):
        self._payload = payload
        self._header  = MAVLink_header(self._header.msgId, len(payload), mav.seq,
                                       mav.srcSystem, mav.srcComponent)
        self._msgbuf = self._header.pack() + payload
        crc = x25crc(self._msgbuf[1:])
        if True: # using CRC extra
            crc.accumulate_str(chr(crc_extra))
        self._crc = crc.crc
        self._msgbuf += struct.pack('<H', self._crc)
        return self._msgbuf


# enums

class EnumEntry(object):
    def __init__(self, name, description):
        self.name = name
        self.description = description
        self.param = {}
        
enums = {}

# MAV_AUTOPILOT
enums['MAV_AUTOPILOT'] = {}
MAV_AUTOPILOT_GENERIC = 0 # Generic autopilot, full support for everything
enums['MAV_AUTOPILOT'][0] = EnumEntry('MAV_AUTOPILOT_GENERIC', '''Generic autopilot, full support for everything''')
MAV_AUTOPILOT_PIXHAWK = 1 # PIXHAWK autopilot, http://pixhawk.ethz.ch
enums['MAV_AUTOPILOT'][1] = EnumEntry('MAV_AUTOPILOT_PIXHAWK', '''PIXHAWK autopilot, http://pixhawk.ethz.ch''')
MAV_AUTOPILOT_SLUGS = 2 # SLUGS autopilot, http://slugsuav.soe.ucsc.edu
enums['MAV_AUTOPILOT'][2] = EnumEntry('MAV_AUTOPILOT_SLUGS', '''SLUGS autopilot, http://slugsuav.soe.ucsc.edu''')
MAV_AUTOPILOT_ARDUPILOTMEGA = 3 # ArduPilotMega / ArduCopter, http://diydrones.com
enums['MAV_AUTOPILOT'][3] = EnumEntry('MAV_AUTOPILOT_ARDUPILOTMEGA', '''ArduPilotMega / ArduCopter, http://diydrones.com''')
MAV_AUTOPILOT_OPENPILOT = 4 # OpenPilot, http://openpilot.org
enums['MAV_AUTOPILOT'][4] = EnumEntry('MAV_AUTOPILOT_OPENPILOT', '''OpenPilot, http://openpilot.org''')
MAV_AUTOPILOT_GENERIC_WAYPOINTS_ONLY = 5 # Generic autopilot only supporting simple waypoints
enums['MAV_AUTOPILOT'][5] = EnumEntry('MAV_AUTOPILOT_GENERIC_WAYPOINTS_ONLY', '''Generic autopilot only supporting simple waypoints''')
MAV_AUTOPILOT_GENERIC_WAYPOINTS_AND_SIMPLE_NAVIGATION_ONLY = 6 # Generic autopilot supporting waypoints and other simple navigation
                        # commands
enums['MAV_AUTOPILOT'][6] = EnumEntry('MAV_AUTOPILOT_GENERIC_WAYPOINTS_AND_SIMPLE_NAVIGATION_ONLY', '''Generic autopilot supporting waypoints and other simple navigation commands''')
MAV_AUTOPILOT_GENERIC_MISSION_FULL = 7 # Generic autopilot supporting the full mission command set
enums['MAV_AUTOPILOT'][7] = EnumEntry('MAV_AUTOPILOT_GENERIC_MISSION_FULL', '''Generic autopilot supporting the full mission command set''')
MAV_AUTOPILOT_INVALID = 8 # No valid autopilot, e.g. a GCS or other MAVLink component
enums['MAV_AUTOPILOT'][8] = EnumEntry('MAV_AUTOPILOT_INVALID', '''No valid autopilot, e.g. a GCS or other MAVLink component''')
MAV_AUTOPILOT_PPZ = 9 # PPZ UAV - http://nongnu.org/paparazzi
enums['MAV_AUTOPILOT'][9] = EnumEntry('MAV_AUTOPILOT_PPZ', '''PPZ UAV - http://nongnu.org/paparazzi''')
MAV_AUTOPILOT_UDB = 10 # UAV Dev Board
enums['MAV_AUTOPILOT'][10] = EnumEntry('MAV_AUTOPILOT_UDB', '''UAV Dev Board''')
MAV_AUTOPILOT_FP = 11 # FlexiPilot
enums['MAV_AUTOPILOT'][11] = EnumEntry('MAV_AUTOPILOT_FP', '''FlexiPilot''')
MAV_AUTOPILOT_PX4 = 12 # PX4 Autopilot - http://pixhawk.ethz.ch/px4/
enums['MAV_AUTOPILOT'][12] = EnumEntry('MAV_AUTOPILOT_PX4', '''PX4 Autopilot - http://pixhawk.ethz.ch/px4/''')
MAV_AUTOPILOT_SMACCMPILOT = 13 # SMACCMPilot - http://smaccmpilot.org
enums['MAV_AUTOPILOT'][13] = EnumEntry('MAV_AUTOPILOT_SMACCMPILOT', '''SMACCMPilot - http://smaccmpilot.org''')
MAV_AUTOPILOT_AUTOQUAD = 14 # AutoQuad -- http://autoquad.org
enums['MAV_AUTOPILOT'][14] = EnumEntry('MAV_AUTOPILOT_AUTOQUAD', '''AutoQuad -- http://autoquad.org''')
MAV_AUTOPILOT_ARMAZILA = 15 # Armazila -- http://armazila.com
enums['MAV_AUTOPILOT'][15] = EnumEntry('MAV_AUTOPILOT_ARMAZILA', '''Armazila -- http://armazila.com''')
MAV_AUTOPILOT_AEROB = 16 # Aerob -- http://aerob.ru
enums['MAV_AUTOPILOT'][16] = EnumEntry('MAV_AUTOPILOT_AEROB', '''Aerob -- http://aerob.ru''')
MAV_AUTOPILOT_ASLUAV = 17 # ASLUAV autopilot -- http://www.asl.ethz.ch
enums['MAV_AUTOPILOT'][17] = EnumEntry('MAV_AUTOPILOT_ASLUAV', '''ASLUAV autopilot -- http://www.asl.ethz.ch''')
MAV_AUTOPILOT_ENUM_END = 18 # 
enums['MAV_AUTOPILOT'][18] = EnumEntry('MAV_AUTOPILOT_ENUM_END', '''''')

# MAV_TYPE
enums['MAV_TYPE'] = {}
MAV_TYPE_GENERIC = 0 # Generic micro air vehicle.
enums['MAV_TYPE'][0] = EnumEntry('MAV_TYPE_GENERIC', '''Generic micro air vehicle.''')
MAV_TYPE_FIXED_WING = 1 # Fixed wing aircraft.
enums['MAV_TYPE'][1] = EnumEntry('MAV_TYPE_FIXED_WING', '''Fixed wing aircraft.''')
MAV_TYPE_QUADROTOR = 2 # Quadrotor
enums['MAV_TYPE'][2] = EnumEntry('MAV_TYPE_QUADROTOR', '''Quadrotor''')
MAV_TYPE_COAXIAL = 3 # Coaxial helicopter
enums['MAV_TYPE'][3] = EnumEntry('MAV_TYPE_COAXIAL', '''Coaxial helicopter''')
MAV_TYPE_HELICOPTER = 4 # Normal helicopter with tail rotor.
enums['MAV_TYPE'][4] = EnumEntry('MAV_TYPE_HELICOPTER', '''Normal helicopter with tail rotor.''')
MAV_TYPE_ANTENNA_TRACKER = 5 # Ground installation
enums['MAV_TYPE'][5] = EnumEntry('MAV_TYPE_ANTENNA_TRACKER', '''Ground installation''')
MAV_TYPE_GCS = 6 # Operator control unit / ground control station
enums['MAV_TYPE'][6] = EnumEntry('MAV_TYPE_GCS', '''Operator control unit / ground control station''')
MAV_TYPE_AIRSHIP = 7 # Airship, controlled
enums['MAV_TYPE'][7] = EnumEntry('MAV_TYPE_AIRSHIP', '''Airship, controlled''')
MAV_TYPE_FREE_BALLOON = 8 # Free balloon, uncontrolled
enums['MAV_TYPE'][8] = EnumEntry('MAV_TYPE_FREE_BALLOON', '''Free balloon, uncontrolled''')
MAV_TYPE_ROCKET = 9 # Rocket
enums['MAV_TYPE'][9] = EnumEntry('MAV_TYPE_ROCKET', '''Rocket''')
MAV_TYPE_GROUND_ROVER = 10 # Ground rover
enums['MAV_TYPE'][10] = EnumEntry('MAV_TYPE_GROUND_ROVER', '''Ground rover''')
MAV_TYPE_SURFACE_BOAT = 11 # Surface vessel, boat, ship
enums['MAV_TYPE'][11] = EnumEntry('MAV_TYPE_SURFACE_BOAT', '''Surface vessel, boat, ship''')
MAV_TYPE_SUBMARINE = 12 # Submarine
enums['MAV_TYPE'][12] = EnumEntry('MAV_TYPE_SUBMARINE', '''Submarine''')
MAV_TYPE_HEXAROTOR = 13 # Hexarotor
enums['MAV_TYPE'][13] = EnumEntry('MAV_TYPE_HEXAROTOR', '''Hexarotor''')
MAV_TYPE_OCTOROTOR = 14 # Octorotor
enums['MAV_TYPE'][14] = EnumEntry('MAV_TYPE_OCTOROTOR', '''Octorotor''')
MAV_TYPE_TRICOPTER = 15 # Octorotor
enums['MAV_TYPE'][15] = EnumEntry('MAV_TYPE_TRICOPTER', '''Octorotor''')
MAV_TYPE_FLAPPING_WING = 16 # Flapping wing
enums['MAV_TYPE'][16] = EnumEntry('MAV_TYPE_FLAPPING_WING', '''Flapping wing''')
MAV_TYPE_KITE = 17 # Flapping wing
enums['MAV_TYPE'][17] = EnumEntry('MAV_TYPE_KITE', '''Flapping wing''')
MAV_TYPE_ONBOARD_CONTROLLER = 18 # Onboard companion controller
enums['MAV_TYPE'][18] = EnumEntry('MAV_TYPE_ONBOARD_CONTROLLER', '''Onboard companion controller''')
MAV_TYPE_VTOL_DUOROTOR = 19 # Two-rotor VTOL using control surfaces in vertical operation in
                        # addition. Tailsitter.
enums['MAV_TYPE'][19] = EnumEntry('MAV_TYPE_VTOL_DUOROTOR', '''Two-rotor VTOL using control surfaces in vertical operation in addition. Tailsitter.''')
MAV_TYPE_VTOL_QUADROTOR = 20 # Quad-rotor VTOL using a V-shaped quad config in vertical operation.
                        # Tailsitter.
enums['MAV_TYPE'][20] = EnumEntry('MAV_TYPE_VTOL_QUADROTOR', '''Quad-rotor VTOL using a V-shaped quad config in vertical operation. Tailsitter.''')
MAV_TYPE_VTOL_RESERVED1 = 21 # VTOL reserved 1
enums['MAV_TYPE'][21] = EnumEntry('MAV_TYPE_VTOL_RESERVED1', '''VTOL reserved 1''')
MAV_TYPE_VTOL_RESERVED2 = 22 # VTOL reserved 2
enums['MAV_TYPE'][22] = EnumEntry('MAV_TYPE_VTOL_RESERVED2', '''VTOL reserved 2''')
MAV_TYPE_VTOL_RESERVED3 = 23 # VTOL reserved 3
enums['MAV_TYPE'][23] = EnumEntry('MAV_TYPE_VTOL_RESERVED3', '''VTOL reserved 3''')
MAV_TYPE_VTOL_RESERVED4 = 24 # VTOL reserved 4
enums['MAV_TYPE'][24] = EnumEntry('MAV_TYPE_VTOL_RESERVED4', '''VTOL reserved 4''')
MAV_TYPE_VTOL_RESERVED5 = 25 # VTOL reserved 5
enums['MAV_TYPE'][25] = EnumEntry('MAV_TYPE_VTOL_RESERVED5', '''VTOL reserved 5''')
MAV_TYPE_GIMBAL = 26 # Onboard gimbal
enums['MAV_TYPE'][26] = EnumEntry('MAV_TYPE_GIMBAL', '''Onboard gimbal''')
MAV_TYPE_ENUM_END = 27 # 
enums['MAV_TYPE'][27] = EnumEntry('MAV_TYPE_ENUM_END', '''''')

# MAV_MODE_FLAG
enums['MAV_MODE_FLAG'] = {}
MAV_MODE_FLAG_CUSTOM_MODE_ENABLED = 1 # 0b00000001 Reserved for future use.
enums['MAV_MODE_FLAG'][1] = EnumEntry('MAV_MODE_FLAG_CUSTOM_MODE_ENABLED', '''0b00000001 Reserved for future use.''')
MAV_MODE_FLAG_TEST_ENABLED = 2 # 0b00000010 system has a test mode enabled. This flag is intended for
                        # temporary system tests and should not be
                        # used for stable implementations.
enums['MAV_MODE_FLAG'][2] = EnumEntry('MAV_MODE_FLAG_TEST_ENABLED', '''0b00000010 system has a test mode enabled. This flag is intended for temporary system tests and should not be used for stable implementations.''')
MAV_MODE_FLAG_AUTO_ENABLED = 4 # 0b00000100 autonomous mode enabled, system finds its own goal
                        # positions. Guided flag can be set or not,
                        # depends on the actual implementation.
enums['MAV_MODE_FLAG'][4] = EnumEntry('MAV_MODE_FLAG_AUTO_ENABLED', '''0b00000100 autonomous mode enabled, system finds its own goal positions. Guided flag can be set or not, depends on the actual implementation.''')
MAV_MODE_FLAG_GUIDED_ENABLED = 8 # 0b00001000 guided mode enabled, system flies MISSIONs / mission items.
enums['MAV_MODE_FLAG'][8] = EnumEntry('MAV_MODE_FLAG_GUIDED_ENABLED', '''0b00001000 guided mode enabled, system flies MISSIONs / mission items.''')
MAV_MODE_FLAG_STABILIZE_ENABLED = 16 # 0b00010000 system stabilizes electronically its attitude (and
                        # optionally position). It needs however
                        # further control inputs to move around.
enums['MAV_MODE_FLAG'][16] = EnumEntry('MAV_MODE_FLAG_STABILIZE_ENABLED', '''0b00010000 system stabilizes electronically its attitude (and optionally position). It needs however further control inputs to move around.''')
MAV_MODE_FLAG_HIL_ENABLED = 32 # 0b00100000 hardware in the loop simulation. All motors / actuators are
                        # blocked, but internal software is full
                        # operational.
enums['MAV_MODE_FLAG'][32] = EnumEntry('MAV_MODE_FLAG_HIL_ENABLED', '''0b00100000 hardware in the loop simulation. All motors / actuators are blocked, but internal software is full operational.''')
MAV_MODE_FLAG_MANUAL_INPUT_ENABLED = 64 # 0b01000000 remote control input is enabled.
enums['MAV_MODE_FLAG'][64] = EnumEntry('MAV_MODE_FLAG_MANUAL_INPUT_ENABLED', '''0b01000000 remote control input is enabled.''')
MAV_MODE_FLAG_SAFETY_ARMED = 128 # 0b10000000 MAV safety set to armed. Motors are enabled / running / can
                        # start. Ready to fly.
enums['MAV_MODE_FLAG'][128] = EnumEntry('MAV_MODE_FLAG_SAFETY_ARMED', '''0b10000000 MAV safety set to armed. Motors are enabled / running / can start. Ready to fly.''')
MAV_MODE_FLAG_ENUM_END = 129 # 
enums['MAV_MODE_FLAG'][129] = EnumEntry('MAV_MODE_FLAG_ENUM_END', '''''')

# MAV_MODE_FLAG_DECODE_POSITION
enums['MAV_MODE_FLAG_DECODE_POSITION'] = {}
MAV_MODE_FLAG_DECODE_POSITION_CUSTOM_MODE = 1 # Eighth bit: 00000001
enums['MAV_MODE_FLAG_DECODE_POSITION'][1] = EnumEntry('MAV_MODE_FLAG_DECODE_POSITION_CUSTOM_MODE', '''Eighth bit: 00000001''')
MAV_MODE_FLAG_DECODE_POSITION_TEST = 2 # Seventh bit: 00000010
enums['MAV_MODE_FLAG_DECODE_POSITION'][2] = EnumEntry('MAV_MODE_FLAG_DECODE_POSITION_TEST', '''Seventh bit: 00000010''')
MAV_MODE_FLAG_DECODE_POSITION_AUTO = 4 # Sixt bit:   00000100
enums['MAV_MODE_FLAG_DECODE_POSITION'][4] = EnumEntry('MAV_MODE_FLAG_DECODE_POSITION_AUTO', '''Sixt bit:   00000100''')
MAV_MODE_FLAG_DECODE_POSITION_GUIDED = 8 # Fifth bit:  00001000
enums['MAV_MODE_FLAG_DECODE_POSITION'][8] = EnumEntry('MAV_MODE_FLAG_DECODE_POSITION_GUIDED', '''Fifth bit:  00001000''')
MAV_MODE_FLAG_DECODE_POSITION_STABILIZE = 16 # Fourth bit: 00010000
enums['MAV_MODE_FLAG_DECODE_POSITION'][16] = EnumEntry('MAV_MODE_FLAG_DECODE_POSITION_STABILIZE', '''Fourth bit: 00010000''')
MAV_MODE_FLAG_DECODE_POSITION_HIL = 32 # Third bit:  00100000
enums['MAV_MODE_FLAG_DECODE_POSITION'][32] = EnumEntry('MAV_MODE_FLAG_DECODE_POSITION_HIL', '''Third bit:  00100000''')
MAV_MODE_FLAG_DECODE_POSITION_MANUAL = 64 # Second bit: 01000000
enums['MAV_MODE_FLAG_DECODE_POSITION'][64] = EnumEntry('MAV_MODE_FLAG_DECODE_POSITION_MANUAL', '''Second bit: 01000000''')
MAV_MODE_FLAG_DECODE_POSITION_SAFETY = 128 # First bit:  10000000
enums['MAV_MODE_FLAG_DECODE_POSITION'][128] = EnumEntry('MAV_MODE_FLAG_DECODE_POSITION_SAFETY', '''First bit:  10000000''')
MAV_MODE_FLAG_DECODE_POSITION_ENUM_END = 129 # 
enums['MAV_MODE_FLAG_DECODE_POSITION'][129] = EnumEntry('MAV_MODE_FLAG_DECODE_POSITION_ENUM_END', '''''')

# MAV_GOTO
enums['MAV_GOTO'] = {}
MAV_GOTO_DO_HOLD = 0 # Hold at the current position.
enums['MAV_GOTO'][0] = EnumEntry('MAV_GOTO_DO_HOLD', '''Hold at the current position.''')
MAV_GOTO_DO_CONTINUE = 1 # Continue with the next item in mission execution.
enums['MAV_GOTO'][1] = EnumEntry('MAV_GOTO_DO_CONTINUE', '''Continue with the next item in mission execution.''')
MAV_GOTO_HOLD_AT_CURRENT_POSITION = 2 # Hold at the current position of the system
enums['MAV_GOTO'][2] = EnumEntry('MAV_GOTO_HOLD_AT_CURRENT_POSITION', '''Hold at the current position of the system''')
MAV_GOTO_HOLD_AT_SPECIFIED_POSITION = 3 # Hold at the position specified in the parameters of the DO_HOLD action
enums['MAV_GOTO'][3] = EnumEntry('MAV_GOTO_HOLD_AT_SPECIFIED_POSITION', '''Hold at the position specified in the parameters of the DO_HOLD action''')
MAV_GOTO_ENUM_END = 4 # 
enums['MAV_GOTO'][4] = EnumEntry('MAV_GOTO_ENUM_END', '''''')

# MAV_MODE
enums['MAV_MODE'] = {}
MAV_MODE_PREFLIGHT = 0 # System is not ready to fly, booting, calibrating, etc. No flag is set.
enums['MAV_MODE'][0] = EnumEntry('MAV_MODE_PREFLIGHT', '''System is not ready to fly, booting, calibrating, etc. No flag is set.''')
MAV_MODE_MANUAL_DISARMED = 64 # System is allowed to be active, under manual (RC) control, no
                        # stabilization
enums['MAV_MODE'][64] = EnumEntry('MAV_MODE_MANUAL_DISARMED', '''System is allowed to be active, under manual (RC) control, no stabilization''')
MAV_MODE_TEST_DISARMED = 66 # UNDEFINED mode. This solely depends on the autopilot - use with
                        # caution, intended for developers only.
enums['MAV_MODE'][66] = EnumEntry('MAV_MODE_TEST_DISARMED', '''UNDEFINED mode. This solely depends on the autopilot - use with caution, intended for developers only.''')
MAV_MODE_STABILIZE_DISARMED = 80 # System is allowed to be active, under assisted RC control.
enums['MAV_MODE'][80] = EnumEntry('MAV_MODE_STABILIZE_DISARMED', '''System is allowed to be active, under assisted RC control.''')
MAV_MODE_GUIDED_DISARMED = 88 # System is allowed to be active, under autonomous control, manual
                        # setpoint
enums['MAV_MODE'][88] = EnumEntry('MAV_MODE_GUIDED_DISARMED', '''System is allowed to be active, under autonomous control, manual setpoint''')
MAV_MODE_AUTO_DISARMED = 92 # System is allowed to be active, under autonomous control and
                        # navigation (the trajectory is decided
                        # onboard and not pre-programmed by MISSIONs)
enums['MAV_MODE'][92] = EnumEntry('MAV_MODE_AUTO_DISARMED', '''System is allowed to be active, under autonomous control and navigation (the trajectory is decided onboard and not pre-programmed by MISSIONs)''')
MAV_MODE_MANUAL_ARMED = 192 # System is allowed to be active, under manual (RC) control, no
                        # stabilization
enums['MAV_MODE'][192] = EnumEntry('MAV_MODE_MANUAL_ARMED', '''System is allowed to be active, under manual (RC) control, no stabilization''')
MAV_MODE_TEST_ARMED = 194 # UNDEFINED mode. This solely depends on the autopilot - use with
                        # caution, intended for developers only.
enums['MAV_MODE'][194] = EnumEntry('MAV_MODE_TEST_ARMED', '''UNDEFINED mode. This solely depends on the autopilot - use with caution, intended for developers only.''')
MAV_MODE_STABILIZE_ARMED = 208 # System is allowed to be active, under assisted RC control.
enums['MAV_MODE'][208] = EnumEntry('MAV_MODE_STABILIZE_ARMED', '''System is allowed to be active, under assisted RC control.''')
MAV_MODE_GUIDED_ARMED = 216 # System is allowed to be active, under autonomous control, manual
                        # setpoint
enums['MAV_MODE'][216] = EnumEntry('MAV_MODE_GUIDED_ARMED', '''System is allowed to be active, under autonomous control, manual setpoint''')
MAV_MODE_AUTO_ARMED = 220 # System is allowed to be active, under autonomous control and
                        # navigation (the trajectory is decided
                        # onboard and not pre-programmed by MISSIONs)
enums['MAV_MODE'][220] = EnumEntry('MAV_MODE_AUTO_ARMED', '''System is allowed to be active, under autonomous control and navigation (the trajectory is decided onboard and not pre-programmed by MISSIONs)''')
MAV_MODE_ENUM_END = 221 # 
enums['MAV_MODE'][221] = EnumEntry('MAV_MODE_ENUM_END', '''''')

# MAV_STATE
enums['MAV_STATE'] = {}
MAV_STATE_UNINIT = 0 # Uninitialized system, state is unknown.
enums['MAV_STATE'][0] = EnumEntry('MAV_STATE_UNINIT', '''Uninitialized system, state is unknown.''')
MAV_STATE_BOOT = 1 # System is booting up.
enums['MAV_STATE'][1] = EnumEntry('MAV_STATE_BOOT', '''System is booting up.''')
MAV_STATE_CALIBRATING = 2 # System is calibrating and not flight-ready.
enums['MAV_STATE'][2] = EnumEntry('MAV_STATE_CALIBRATING', '''System is calibrating and not flight-ready.''')
MAV_STATE_STANDBY = 3 # System is grounded and on standby. It can be launched any time.
enums['MAV_STATE'][3] = EnumEntry('MAV_STATE_STANDBY', '''System is grounded and on standby. It can be launched any time.''')
MAV_STATE_ACTIVE = 4 # System is active and might be already airborne. Motors are engaged.
enums['MAV_STATE'][4] = EnumEntry('MAV_STATE_ACTIVE', '''System is active and might be already airborne. Motors are engaged.''')
MAV_STATE_CRITICAL = 5 # System is in a non-normal flight mode. It can however still navigate.
enums['MAV_STATE'][5] = EnumEntry('MAV_STATE_CRITICAL', '''System is in a non-normal flight mode. It can however still navigate.''')
MAV_STATE_EMERGENCY = 6 # System is in a non-normal flight mode. It lost control over parts or
                        # over the whole airframe. It is in mayday and
                        # going down.
enums['MAV_STATE'][6] = EnumEntry('MAV_STATE_EMERGENCY', '''System is in a non-normal flight mode. It lost control over parts or over the whole airframe. It is in mayday and going down.''')
MAV_STATE_POWEROFF = 7 # System just initialized its power-down sequence, will shut down now.
enums['MAV_STATE'][7] = EnumEntry('MAV_STATE_POWEROFF', '''System just initialized its power-down sequence, will shut down now.''')
MAV_STATE_ENUM_END = 8 # 
enums['MAV_STATE'][8] = EnumEntry('MAV_STATE_ENUM_END', '''''')

# MAV_COMPONENT
enums['MAV_COMPONENT'] = {}
MAV_COMP_ID_ALL = 0 # 
enums['MAV_COMPONENT'][0] = EnumEntry('MAV_COMP_ID_ALL', '''''')
MAV_COMP_ID_CAMERA = 100 # 
enums['MAV_COMPONENT'][100] = EnumEntry('MAV_COMP_ID_CAMERA', '''''')
MAV_COMP_ID_SERVO1 = 140 # 
enums['MAV_COMPONENT'][140] = EnumEntry('MAV_COMP_ID_SERVO1', '''''')
MAV_COMP_ID_SERVO2 = 141 # 
enums['MAV_COMPONENT'][141] = EnumEntry('MAV_COMP_ID_SERVO2', '''''')
MAV_COMP_ID_SERVO3 = 142 # 
enums['MAV_COMPONENT'][142] = EnumEntry('MAV_COMP_ID_SERVO3', '''''')
MAV_COMP_ID_SERVO4 = 143 # 
enums['MAV_COMPONENT'][143] = EnumEntry('MAV_COMP_ID_SERVO4', '''''')
MAV_COMP_ID_SERVO5 = 144 # 
enums['MAV_COMPONENT'][144] = EnumEntry('MAV_COMP_ID_SERVO5', '''''')
MAV_COMP_ID_SERVO6 = 145 # 
enums['MAV_COMPONENT'][145] = EnumEntry('MAV_COMP_ID_SERVO6', '''''')
MAV_COMP_ID_SERVO7 = 146 # 
enums['MAV_COMPONENT'][146] = EnumEntry('MAV_COMP_ID_SERVO7', '''''')
MAV_COMP_ID_SERVO8 = 147 # 
enums['MAV_COMPONENT'][147] = EnumEntry('MAV_COMP_ID_SERVO8', '''''')
MAV_COMP_ID_SERVO9 = 148 # 
enums['MAV_COMPONENT'][148] = EnumEntry('MAV_COMP_ID_SERVO9', '''''')
MAV_COMP_ID_SERVO10 = 149 # 
enums['MAV_COMPONENT'][149] = EnumEntry('MAV_COMP_ID_SERVO10', '''''')
MAV_COMP_ID_SERVO11 = 150 # 
enums['MAV_COMPONENT'][150] = EnumEntry('MAV_COMP_ID_SERVO11', '''''')
MAV_COMP_ID_SERVO12 = 151 # 
enums['MAV_COMPONENT'][151] = EnumEntry('MAV_COMP_ID_SERVO12', '''''')
MAV_COMP_ID_SERVO13 = 152 # 
enums['MAV_COMPONENT'][152] = EnumEntry('MAV_COMP_ID_SERVO13', '''''')
MAV_COMP_ID_SERVO14 = 153 # 
enums['MAV_COMPONENT'][153] = EnumEntry('MAV_COMP_ID_SERVO14', '''''')
MAV_COMP_ID_GIMBAL = 154 # 
enums['MAV_COMPONENT'][154] = EnumEntry('MAV_COMP_ID_GIMBAL', '''''')
MAV_COMP_ID_MAPPER = 180 # 
enums['MAV_COMPONENT'][180] = EnumEntry('MAV_COMP_ID_MAPPER', '''''')
MAV_COMP_ID_MISSIONPLANNER = 190 # 
enums['MAV_COMPONENT'][190] = EnumEntry('MAV_COMP_ID_MISSIONPLANNER', '''''')
MAV_COMP_ID_PATHPLANNER = 195 # 
enums['MAV_COMPONENT'][195] = EnumEntry('MAV_COMP_ID_PATHPLANNER', '''''')
MAV_COMP_ID_IMU = 200 # 
enums['MAV_COMPONENT'][200] = EnumEntry('MAV_COMP_ID_IMU', '''''')
MAV_COMP_ID_IMU_2 = 201 # 
enums['MAV_COMPONENT'][201] = EnumEntry('MAV_COMP_ID_IMU_2', '''''')
MAV_COMP_ID_IMU_3 = 202 # 
enums['MAV_COMPONENT'][202] = EnumEntry('MAV_COMP_ID_IMU_3', '''''')
MAV_COMP_ID_GPS = 220 # 
enums['MAV_COMPONENT'][220] = EnumEntry('MAV_COMP_ID_GPS', '''''')
MAV_COMP_ID_UDP_BRIDGE = 240 # 
enums['MAV_COMPONENT'][240] = EnumEntry('MAV_COMP_ID_UDP_BRIDGE', '''''')
MAV_COMP_ID_UART_BRIDGE = 241 # 
enums['MAV_COMPONENT'][241] = EnumEntry('MAV_COMP_ID_UART_BRIDGE', '''''')
MAV_COMP_ID_SYSTEM_CONTROL = 250 # 
enums['MAV_COMPONENT'][250] = EnumEntry('MAV_COMP_ID_SYSTEM_CONTROL', '''''')
MAV_COMPONENT_ENUM_END = 251 # 
enums['MAV_COMPONENT'][251] = EnumEntry('MAV_COMPONENT_ENUM_END', '''''')

# MAV_SYS_STATUS_SENSOR
enums['MAV_SYS_STATUS_SENSOR'] = {}
MAV_SYS_STATUS_SENSOR_3D_GYRO = 1 # 0x01 3D gyro
enums['MAV_SYS_STATUS_SENSOR'][1] = EnumEntry('MAV_SYS_STATUS_SENSOR_3D_GYRO', '''0x01 3D gyro''')
MAV_SYS_STATUS_SENSOR_3D_ACCEL = 2 # 0x02 3D accelerometer
enums['MAV_SYS_STATUS_SENSOR'][2] = EnumEntry('MAV_SYS_STATUS_SENSOR_3D_ACCEL', '''0x02 3D accelerometer''')
MAV_SYS_STATUS_SENSOR_3D_MAG = 4 # 0x04 3D magnetometer
enums['MAV_SYS_STATUS_SENSOR'][4] = EnumEntry('MAV_SYS_STATUS_SENSOR_3D_MAG', '''0x04 3D magnetometer''')
MAV_SYS_STATUS_SENSOR_ABSOLUTE_PRESSURE = 8 # 0x08 absolute pressure
enums['MAV_SYS_STATUS_SENSOR'][8] = EnumEntry('MAV_SYS_STATUS_SENSOR_ABSOLUTE_PRESSURE', '''0x08 absolute pressure''')
MAV_SYS_STATUS_SENSOR_DIFFERENTIAL_PRESSURE = 16 # 0x10 differential pressure
enums['MAV_SYS_STATUS_SENSOR'][16] = EnumEntry('MAV_SYS_STATUS_SENSOR_DIFFERENTIAL_PRESSURE', '''0x10 differential pressure''')
MAV_SYS_STATUS_SENSOR_GPS = 32 # 0x20 GPS
enums['MAV_SYS_STATUS_SENSOR'][32] = EnumEntry('MAV_SYS_STATUS_SENSOR_GPS', '''0x20 GPS''')
MAV_SYS_STATUS_SENSOR_OPTICAL_FLOW = 64 # 0x40 optical flow
enums['MAV_SYS_STATUS_SENSOR'][64] = EnumEntry('MAV_SYS_STATUS_SENSOR_OPTICAL_FLOW', '''0x40 optical flow''')
MAV_SYS_STATUS_SENSOR_VISION_POSITION = 128 # 0x80 computer vision position
enums['MAV_SYS_STATUS_SENSOR'][128] = EnumEntry('MAV_SYS_STATUS_SENSOR_VISION_POSITION', '''0x80 computer vision position''')
MAV_SYS_STATUS_SENSOR_LASER_POSITION = 256 # 0x100 laser based position
enums['MAV_SYS_STATUS_SENSOR'][256] = EnumEntry('MAV_SYS_STATUS_SENSOR_LASER_POSITION', '''0x100 laser based position''')
MAV_SYS_STATUS_SENSOR_EXTERNAL_GROUND_TRUTH = 512 # 0x200 external ground truth (Vicon or Leica)
enums['MAV_SYS_STATUS_SENSOR'][512] = EnumEntry('MAV_SYS_STATUS_SENSOR_EXTERNAL_GROUND_TRUTH', '''0x200 external ground truth (Vicon or Leica)''')
MAV_SYS_STATUS_SENSOR_ANGULAR_RATE_CONTROL = 1024 # 0x400 3D angular rate control
enums['MAV_SYS_STATUS_SENSOR'][1024] = EnumEntry('MAV_SYS_STATUS_SENSOR_ANGULAR_RATE_CONTROL', '''0x400 3D angular rate control''')
MAV_SYS_STATUS_SENSOR_ATTITUDE_STABILIZATION = 2048 # 0x800 attitude stabilization
enums['MAV_SYS_STATUS_SENSOR'][2048] = EnumEntry('MAV_SYS_STATUS_SENSOR_ATTITUDE_STABILIZATION', '''0x800 attitude stabilization''')
MAV_SYS_STATUS_SENSOR_YAW_POSITION = 4096 # 0x1000 yaw position
enums['MAV_SYS_STATUS_SENSOR'][4096] = EnumEntry('MAV_SYS_STATUS_SENSOR_YAW_POSITION', '''0x1000 yaw position''')
MAV_SYS_STATUS_SENSOR_Z_ALTITUDE_CONTROL = 8192 # 0x2000 z/altitude control
enums['MAV_SYS_STATUS_SENSOR'][8192] = EnumEntry('MAV_SYS_STATUS_SENSOR_Z_ALTITUDE_CONTROL', '''0x2000 z/altitude control''')
MAV_SYS_STATUS_SENSOR_XY_POSITION_CONTROL = 16384 # 0x4000 x/y position control
enums['MAV_SYS_STATUS_SENSOR'][16384] = EnumEntry('MAV_SYS_STATUS_SENSOR_XY_POSITION_CONTROL', '''0x4000 x/y position control''')
MAV_SYS_STATUS_SENSOR_MOTOR_OUTPUTS = 32768 # 0x8000 motor outputs / control
enums['MAV_SYS_STATUS_SENSOR'][32768] = EnumEntry('MAV_SYS_STATUS_SENSOR_MOTOR_OUTPUTS', '''0x8000 motor outputs / control''')
MAV_SYS_STATUS_SENSOR_RC_RECEIVER = 65536 # 0x10000 rc receiver
enums['MAV_SYS_STATUS_SENSOR'][65536] = EnumEntry('MAV_SYS_STATUS_SENSOR_RC_RECEIVER', '''0x10000 rc receiver''')
MAV_SYS_STATUS_SENSOR_3D_GYRO2 = 131072 # 0x20000 2nd 3D gyro
enums['MAV_SYS_STATUS_SENSOR'][131072] = EnumEntry('MAV_SYS_STATUS_SENSOR_3D_GYRO2', '''0x20000 2nd 3D gyro''')
MAV_SYS_STATUS_SENSOR_3D_ACCEL2 = 262144 # 0x40000 2nd 3D accelerometer
enums['MAV_SYS_STATUS_SENSOR'][262144] = EnumEntry('MAV_SYS_STATUS_SENSOR_3D_ACCEL2', '''0x40000 2nd 3D accelerometer''')
MAV_SYS_STATUS_SENSOR_3D_MAG2 = 524288 # 0x80000 2nd 3D magnetometer
enums['MAV_SYS_STATUS_SENSOR'][524288] = EnumEntry('MAV_SYS_STATUS_SENSOR_3D_MAG2', '''0x80000 2nd 3D magnetometer''')
MAV_SYS_STATUS_GEOFENCE = 1048576 # 0x100000 geofence
enums['MAV_SYS_STATUS_SENSOR'][1048576] = EnumEntry('MAV_SYS_STATUS_GEOFENCE', '''0x100000 geofence''')
MAV_SYS_STATUS_AHRS = 2097152 # 0x200000 AHRS subsystem health
enums['MAV_SYS_STATUS_SENSOR'][2097152] = EnumEntry('MAV_SYS_STATUS_AHRS', '''0x200000 AHRS subsystem health''')
MAV_SYS_STATUS_TERRAIN = 4194304 # 0x400000 Terrain subsystem health
enums['MAV_SYS_STATUS_SENSOR'][4194304] = EnumEntry('MAV_SYS_STATUS_TERRAIN', '''0x400000 Terrain subsystem health''')
MAV_SYS_STATUS_SENSOR_ENUM_END = 4194305 # 
enums['MAV_SYS_STATUS_SENSOR'][4194305] = EnumEntry('MAV_SYS_STATUS_SENSOR_ENUM_END', '''''')

# MAV_FRAME
enums['MAV_FRAME'] = {}
MAV_FRAME_GLOBAL = 0 # Global coordinate frame, WGS84 coordinate system. First value / x:
                        # latitude, second value / y: longitude, third
                        # value / z: positive altitude over mean sea
                        # level (MSL)
enums['MAV_FRAME'][0] = EnumEntry('MAV_FRAME_GLOBAL', '''Global coordinate frame, WGS84 coordinate system. First value / x: latitude, second value / y: longitude, third value / z: positive altitude over mean sea level (MSL)''')
MAV_FRAME_LOCAL_NED = 1 # Local coordinate frame, Z-up (x: north, y: east, z: down).
enums['MAV_FRAME'][1] = EnumEntry('MAV_FRAME_LOCAL_NED', '''Local coordinate frame, Z-up (x: north, y: east, z: down).''')
MAV_FRAME_MISSION = 2 # NOT a coordinate frame, indicates a mission command.
enums['MAV_FRAME'][2] = EnumEntry('MAV_FRAME_MISSION', '''NOT a coordinate frame, indicates a mission command.''')
MAV_FRAME_GLOBAL_RELATIVE_ALT = 3 # Global coordinate frame, WGS84 coordinate system, relative altitude
                        # over ground with respect to the home
                        # position. First value / x: latitude, second
                        # value / y: longitude, third value / z:
                        # positive altitude with 0 being at the
                        # altitude of the home location.
enums['MAV_FRAME'][3] = EnumEntry('MAV_FRAME_GLOBAL_RELATIVE_ALT', '''Global coordinate frame, WGS84 coordinate system, relative altitude over ground with respect to the home position. First value / x: latitude, second value / y: longitude, third value / z: positive altitude with 0 being at the altitude of the home location.''')
MAV_FRAME_LOCAL_ENU = 4 # Local coordinate frame, Z-down (x: east, y: north, z: up)
enums['MAV_FRAME'][4] = EnumEntry('MAV_FRAME_LOCAL_ENU', '''Local coordinate frame, Z-down (x: east, y: north, z: up)''')
MAV_FRAME_GLOBAL_INT = 5 # Global coordinate frame, WGS84 coordinate system. First value / x:
                        # latitude in degrees*1.0e-7, second value /
                        # y: longitude in degrees*1.0e-7, third value
                        # / z: positive altitude over mean sea level
                        # (MSL)
enums['MAV_FRAME'][5] = EnumEntry('MAV_FRAME_GLOBAL_INT', '''Global coordinate frame, WGS84 coordinate system. First value / x: latitude in degrees*1.0e-7, second value / y: longitude in degrees*1.0e-7, third value / z: positive altitude over mean sea level (MSL)''')
MAV_FRAME_GLOBAL_RELATIVE_ALT_INT = 6 # Global coordinate frame, WGS84 coordinate system, relative altitude
                        # over ground with respect to the home
                        # position. First value / x: latitude in
                        # degrees*10e-7, second value / y: longitude
                        # in degrees*10e-7, third value / z: positive
                        # altitude with 0 being at the altitude of the
                        # home location.
enums['MAV_FRAME'][6] = EnumEntry('MAV_FRAME_GLOBAL_RELATIVE_ALT_INT', '''Global coordinate frame, WGS84 coordinate system, relative altitude over ground with respect to the home position. First value / x: latitude in degrees*10e-7, second value / y: longitude in degrees*10e-7, third value / z: positive altitude with 0 being at the altitude of the home location.''')
MAV_FRAME_LOCAL_OFFSET_NED = 7 # Offset to the current local frame. Anything expressed in this frame
                        # should be added to the current local frame
                        # position.
enums['MAV_FRAME'][7] = EnumEntry('MAV_FRAME_LOCAL_OFFSET_NED', '''Offset to the current local frame. Anything expressed in this frame should be added to the current local frame position.''')
MAV_FRAME_BODY_NED = 8 # Setpoint in body NED frame. This makes sense if all position control
                        # is externalized - e.g. useful to command 2
                        # m/s^2 acceleration to the right.
enums['MAV_FRAME'][8] = EnumEntry('MAV_FRAME_BODY_NED', '''Setpoint in body NED frame. This makes sense if all position control is externalized - e.g. useful to command 2 m/s^2 acceleration to the right.''')
MAV_FRAME_BODY_OFFSET_NED = 9 # Offset in body NED frame. This makes sense if adding setpoints to the
                        # current flight path, to avoid an obstacle -
                        # e.g. useful to command 2 m/s^2 acceleration
                        # to the east.
enums['MAV_FRAME'][9] = EnumEntry('MAV_FRAME_BODY_OFFSET_NED', '''Offset in body NED frame. This makes sense if adding setpoints to the current flight path, to avoid an obstacle - e.g. useful to command 2 m/s^2 acceleration to the east.''')
MAV_FRAME_GLOBAL_TERRAIN_ALT = 10 # Global coordinate frame with above terrain level altitude. WGS84
                        # coordinate system, relative altitude over
                        # terrain with respect to the waypoint
                        # coordinate. First value / x: latitude in
                        # degrees, second value / y: longitude in
                        # degrees, third value / z: positive altitude
                        # in meters with 0 being at ground level in
                        # terrain model.
enums['MAV_FRAME'][10] = EnumEntry('MAV_FRAME_GLOBAL_TERRAIN_ALT', '''Global coordinate frame with above terrain level altitude. WGS84 coordinate system, relative altitude over terrain with respect to the waypoint coordinate. First value / x: latitude in degrees, second value / y: longitude in degrees, third value / z: positive altitude in meters with 0 being at ground level in terrain model.''')
MAV_FRAME_GLOBAL_TERRAIN_ALT_INT = 11 # Global coordinate frame with above terrain level altitude. WGS84
                        # coordinate system, relative altitude over
                        # terrain with respect to the waypoint
                        # coordinate. First value / x: latitude in
                        # degrees*10e-7, second value / y: longitude
                        # in degrees*10e-7, third value / z: positive
                        # altitude in meters with 0 being at ground
                        # level in terrain model.
enums['MAV_FRAME'][11] = EnumEntry('MAV_FRAME_GLOBAL_TERRAIN_ALT_INT', '''Global coordinate frame with above terrain level altitude. WGS84 coordinate system, relative altitude over terrain with respect to the waypoint coordinate. First value / x: latitude in degrees*10e-7, second value / y: longitude in degrees*10e-7, third value / z: positive altitude in meters with 0 being at ground level in terrain model.''')
MAV_FRAME_ENUM_END = 12 # 
enums['MAV_FRAME'][12] = EnumEntry('MAV_FRAME_ENUM_END', '''''')

# MAVLINK_DATA_STREAM_TYPE
enums['MAVLINK_DATA_STREAM_TYPE'] = {}
MAVLINK_DATA_STREAM_IMG_JPEG = 1 # 
enums['MAVLINK_DATA_STREAM_TYPE'][1] = EnumEntry('MAVLINK_DATA_STREAM_IMG_JPEG', '''''')
MAVLINK_DATA_STREAM_IMG_BMP = 2 # 
enums['MAVLINK_DATA_STREAM_TYPE'][2] = EnumEntry('MAVLINK_DATA_STREAM_IMG_BMP', '''''')
MAVLINK_DATA_STREAM_IMG_RAW8U = 3 # 
enums['MAVLINK_DATA_STREAM_TYPE'][3] = EnumEntry('MAVLINK_DATA_STREAM_IMG_RAW8U', '''''')
MAVLINK_DATA_STREAM_IMG_RAW32U = 4 # 
enums['MAVLINK_DATA_STREAM_TYPE'][4] = EnumEntry('MAVLINK_DATA_STREAM_IMG_RAW32U', '''''')
MAVLINK_DATA_STREAM_IMG_PGM = 5 # 
enums['MAVLINK_DATA_STREAM_TYPE'][5] = EnumEntry('MAVLINK_DATA_STREAM_IMG_PGM', '''''')
MAVLINK_DATA_STREAM_IMG_PNG = 6 # 
enums['MAVLINK_DATA_STREAM_TYPE'][6] = EnumEntry('MAVLINK_DATA_STREAM_IMG_PNG', '''''')
MAVLINK_DATA_STREAM_TYPE_ENUM_END = 7 # 
enums['MAVLINK_DATA_STREAM_TYPE'][7] = EnumEntry('MAVLINK_DATA_STREAM_TYPE_ENUM_END', '''''')

# FENCE_ACTION
enums['FENCE_ACTION'] = {}
FENCE_ACTION_NONE = 0 # Disable fenced mode
enums['FENCE_ACTION'][0] = EnumEntry('FENCE_ACTION_NONE', '''Disable fenced mode''')
FENCE_ACTION_GUIDED = 1 # Switched to guided mode to return point (fence point 0)
enums['FENCE_ACTION'][1] = EnumEntry('FENCE_ACTION_GUIDED', '''Switched to guided mode to return point (fence point 0)''')
FENCE_ACTION_REPORT = 2 # Report fence breach, but don't take action
enums['FENCE_ACTION'][2] = EnumEntry('FENCE_ACTION_REPORT', '''Report fence breach, but don't take action''')
FENCE_ACTION_GUIDED_THR_PASS = 3 # Switched to guided mode to return point (fence point 0) with manual
                        # throttle control
enums['FENCE_ACTION'][3] = EnumEntry('FENCE_ACTION_GUIDED_THR_PASS', '''Switched to guided mode to return point (fence point 0) with manual throttle control''')
FENCE_ACTION_ENUM_END = 4 # 
enums['FENCE_ACTION'][4] = EnumEntry('FENCE_ACTION_ENUM_END', '''''')

# FENCE_BREACH
enums['FENCE_BREACH'] = {}
FENCE_BREACH_NONE = 0 # No last fence breach
enums['FENCE_BREACH'][0] = EnumEntry('FENCE_BREACH_NONE', '''No last fence breach''')
FENCE_BREACH_MINALT = 1 # Breached minimum altitude
enums['FENCE_BREACH'][1] = EnumEntry('FENCE_BREACH_MINALT', '''Breached minimum altitude''')
FENCE_BREACH_MAXALT = 2 # Breached maximum altitude
enums['FENCE_BREACH'][2] = EnumEntry('FENCE_BREACH_MAXALT', '''Breached maximum altitude''')
FENCE_BREACH_BOUNDARY = 3 # Breached fence boundary
enums['FENCE_BREACH'][3] = EnumEntry('FENCE_BREACH_BOUNDARY', '''Breached fence boundary''')
FENCE_BREACH_ENUM_END = 4 # 
enums['FENCE_BREACH'][4] = EnumEntry('FENCE_BREACH_ENUM_END', '''''')

# MAV_MOUNT_MODE
enums['MAV_MOUNT_MODE'] = {}
MAV_MOUNT_MODE_RETRACT = 0 # Load and keep safe position (Roll,Pitch,Yaw) from permant memory and
                        # stop stabilization
enums['MAV_MOUNT_MODE'][0] = EnumEntry('MAV_MOUNT_MODE_RETRACT', '''Load and keep safe position (Roll,Pitch,Yaw) from permant memory and stop stabilization''')
MAV_MOUNT_MODE_NEUTRAL = 1 # Load and keep neutral position (Roll,Pitch,Yaw) from permanent memory.
enums['MAV_MOUNT_MODE'][1] = EnumEntry('MAV_MOUNT_MODE_NEUTRAL', '''Load and keep neutral position (Roll,Pitch,Yaw) from permanent memory.''')
MAV_MOUNT_MODE_MAVLINK_TARGETING = 2 # Load neutral position and start MAVLink Roll,Pitch,Yaw control with
                        # stabilization
enums['MAV_MOUNT_MODE'][2] = EnumEntry('MAV_MOUNT_MODE_MAVLINK_TARGETING', '''Load neutral position and start MAVLink Roll,Pitch,Yaw control with stabilization''')
MAV_MOUNT_MODE_RC_TARGETING = 3 # Load neutral position and start RC Roll,Pitch,Yaw control with
                        # stabilization
enums['MAV_MOUNT_MODE'][3] = EnumEntry('MAV_MOUNT_MODE_RC_TARGETING', '''Load neutral position and start RC Roll,Pitch,Yaw control with stabilization''')
MAV_MOUNT_MODE_GPS_POINT = 4 # Load neutral position and start to point to Lat,Lon,Alt
enums['MAV_MOUNT_MODE'][4] = EnumEntry('MAV_MOUNT_MODE_GPS_POINT', '''Load neutral position and start to point to Lat,Lon,Alt''')
MAV_MOUNT_MODE_ENUM_END = 5 # 
enums['MAV_MOUNT_MODE'][5] = EnumEntry('MAV_MOUNT_MODE_ENUM_END', '''''')

# MAV_CMD
enums['MAV_CMD'] = {}
MAV_CMD_NAV_WAYPOINT = 16 # Navigate to MISSION.
enums['MAV_CMD'][16] = EnumEntry('MAV_CMD_NAV_WAYPOINT', '''Navigate to MISSION.''')
enums['MAV_CMD'][16].param[1] = '''Hold time in decimal seconds. (ignored by fixed wing, time to stay at MISSION for rotary wing)'''
enums['MAV_CMD'][16].param[2] = '''Acceptance radius in meters (if the sphere with this radius is hit, the MISSION counts as reached)'''
enums['MAV_CMD'][16].param[3] = '''0 to pass through the WP, if > 0 radius in meters to pass by WP. Positive value for clockwise orbit, negative value for counter-clockwise orbit. Allows trajectory control.'''
enums['MAV_CMD'][16].param[4] = '''Desired yaw angle at MISSION (rotary wing)'''
enums['MAV_CMD'][16].param[5] = '''Latitude'''
enums['MAV_CMD'][16].param[6] = '''Longitude'''
enums['MAV_CMD'][16].param[7] = '''Altitude'''
MAV_CMD_NAV_LOITER_UNLIM = 17 # Loiter around this MISSION an unlimited amount of time
enums['MAV_CMD'][17] = EnumEntry('MAV_CMD_NAV_LOITER_UNLIM', '''Loiter around this MISSION an unlimited amount of time''')
enums['MAV_CMD'][17].param[1] = '''Empty'''
enums['MAV_CMD'][17].param[2] = '''Empty'''
enums['MAV_CMD'][17].param[3] = '''Radius around MISSION, in meters. If positive loiter clockwise, else counter-clockwise'''
enums['MAV_CMD'][17].param[4] = '''Desired yaw angle.'''
enums['MAV_CMD'][17].param[5] = '''Latitude'''
enums['MAV_CMD'][17].param[6] = '''Longitude'''
enums['MAV_CMD'][17].param[7] = '''Altitude'''
MAV_CMD_NAV_LOITER_TURNS = 18 # Loiter around this MISSION for X turns
enums['MAV_CMD'][18] = EnumEntry('MAV_CMD_NAV_LOITER_TURNS', '''Loiter around this MISSION for X turns''')
enums['MAV_CMD'][18].param[1] = '''Turns'''
enums['MAV_CMD'][18].param[2] = '''Empty'''
enums['MAV_CMD'][18].param[3] = '''Radius around MISSION, in meters. If positive loiter clockwise, else counter-clockwise'''
enums['MAV_CMD'][18].param[4] = '''Desired yaw angle.'''
enums['MAV_CMD'][18].param[5] = '''Latitude'''
enums['MAV_CMD'][18].param[6] = '''Longitude'''
enums['MAV_CMD'][18].param[7] = '''Altitude'''
MAV_CMD_NAV_LOITER_TIME = 19 # Loiter around this MISSION for X seconds
enums['MAV_CMD'][19] = EnumEntry('MAV_CMD_NAV_LOITER_TIME', '''Loiter around this MISSION for X seconds''')
enums['MAV_CMD'][19].param[1] = '''Seconds (decimal)'''
enums['MAV_CMD'][19].param[2] = '''Empty'''
enums['MAV_CMD'][19].param[3] = '''Radius around MISSION, in meters. If positive loiter clockwise, else counter-clockwise'''
enums['MAV_CMD'][19].param[4] = '''Desired yaw angle.'''
enums['MAV_CMD'][19].param[5] = '''Latitude'''
enums['MAV_CMD'][19].param[6] = '''Longitude'''
enums['MAV_CMD'][19].param[7] = '''Altitude'''
MAV_CMD_NAV_RETURN_TO_LAUNCH = 20 # Return to launch location
enums['MAV_CMD'][20] = EnumEntry('MAV_CMD_NAV_RETURN_TO_LAUNCH', '''Return to launch location''')
enums['MAV_CMD'][20].param[1] = '''Empty'''
enums['MAV_CMD'][20].param[2] = '''Empty'''
enums['MAV_CMD'][20].param[3] = '''Empty'''
enums['MAV_CMD'][20].param[4] = '''Empty'''
enums['MAV_CMD'][20].param[5] = '''Empty'''
enums['MAV_CMD'][20].param[6] = '''Empty'''
enums['MAV_CMD'][20].param[7] = '''Empty'''
MAV_CMD_NAV_LAND = 21 # Land at location
enums['MAV_CMD'][21] = EnumEntry('MAV_CMD_NAV_LAND', '''Land at location''')
enums['MAV_CMD'][21].param[1] = '''Empty'''
enums['MAV_CMD'][21].param[2] = '''Empty'''
enums['MAV_CMD'][21].param[3] = '''Empty'''
enums['MAV_CMD'][21].param[4] = '''Desired yaw angle'''
enums['MAV_CMD'][21].param[5] = '''Latitude'''
enums['MAV_CMD'][21].param[6] = '''Longitude'''
enums['MAV_CMD'][21].param[7] = '''Altitude'''
MAV_CMD_NAV_TAKEOFF = 22 # Takeoff from ground / hand
enums['MAV_CMD'][22] = EnumEntry('MAV_CMD_NAV_TAKEOFF', '''Takeoff from ground / hand''')
enums['MAV_CMD'][22].param[1] = '''Minimum pitch (if airspeed sensor present), desired pitch without sensor'''
enums['MAV_CMD'][22].param[2] = '''Empty'''
enums['MAV_CMD'][22].param[3] = '''Empty'''
enums['MAV_CMD'][22].param[4] = '''Yaw angle (if magnetometer present), ignored without magnetometer'''
enums['MAV_CMD'][22].param[5] = '''Latitude'''
enums['MAV_CMD'][22].param[6] = '''Longitude'''
enums['MAV_CMD'][22].param[7] = '''Altitude'''
MAV_CMD_NAV_LAND_LOCAL = 23 # Land at local position (local frame only)
enums['MAV_CMD'][23] = EnumEntry('MAV_CMD_NAV_LAND_LOCAL', '''Land at local position (local frame only)''')
enums['MAV_CMD'][23].param[1] = '''Landing target number (if available)'''
enums['MAV_CMD'][23].param[2] = '''Maximum accepted offset from desired landing position [m] - computed magnitude from spherical coordinates: d = sqrt(x^2 + y^2 + z^2), which gives the maximum accepted distance between the desired landing position and the position where the vehicle is about to land'''
enums['MAV_CMD'][23].param[3] = '''Landing descend rate [ms^-1]'''
enums['MAV_CMD'][23].param[4] = '''Desired yaw angle [rad]'''
enums['MAV_CMD'][23].param[5] = '''Y-axis position [m]'''
enums['MAV_CMD'][23].param[6] = '''X-axis position [m]'''
enums['MAV_CMD'][23].param[7] = '''Z-axis / ground level position [m]'''
MAV_CMD_NAV_TAKEOFF_LOCAL = 24 # Takeoff from local position (local frame only)
enums['MAV_CMD'][24] = EnumEntry('MAV_CMD_NAV_TAKEOFF_LOCAL', '''Takeoff from local position (local frame only)''')
enums['MAV_CMD'][24].param[1] = '''Minimum pitch (if airspeed sensor present), desired pitch without sensor [rad]'''
enums['MAV_CMD'][24].param[2] = '''Empty'''
enums['MAV_CMD'][24].param[3] = '''Takeoff ascend rate [ms^-1]'''
enums['MAV_CMD'][24].param[4] = '''Yaw angle [rad] (if magnetometer or another yaw estimation source present), ignored without one of these'''
enums['MAV_CMD'][24].param[5] = '''Y-axis position [m]'''
enums['MAV_CMD'][24].param[6] = '''X-axis position [m]'''
enums['MAV_CMD'][24].param[7] = '''Z-axis position [m]'''
MAV_CMD_NAV_CONTINUE_AND_CHANGE_ALT = 30 # Continue on the current course and climb/descend to specified
                        # altitude.  When the altitude is reached
                        # continue to the next command (i.e., don't
                        # proceed to the next command until the
                        # desired altitude is reached.
enums['MAV_CMD'][30] = EnumEntry('MAV_CMD_NAV_CONTINUE_AND_CHANGE_ALT', '''Continue on the current course and climb/descend to specified altitude.  When the altitude is reached continue to the next command (i.e., don't proceed to the next command until the desired altitude is reached.''')
enums['MAV_CMD'][30].param[1] = '''Empty'''
enums['MAV_CMD'][30].param[2] = '''Empty'''
enums['MAV_CMD'][30].param[3] = '''Empty'''
enums['MAV_CMD'][30].param[4] = '''Empty'''
enums['MAV_CMD'][30].param[5] = '''Empty'''
enums['MAV_CMD'][30].param[6] = '''Empty'''
enums['MAV_CMD'][30].param[7] = '''Desired altitude in meters'''
MAV_CMD_NAV_LOITER_TO_ALT = 31 # Begin loiter at the specified Latitude and Longitude.  If Lat=Lon=0,
                        # then loiter at the current position.  Don't
                        # consider the navigation command complete
                        # (don't leave loiter) until the altitude has
                        # been reached.  Additionally, if the Heading
                        # Required parameter is non-zero the  aircraft
                        # will not leave the loiter until heading
                        # toward the next waypoint.
enums['MAV_CMD'][31] = EnumEntry('MAV_CMD_NAV_LOITER_TO_ALT', '''Begin loiter at the specified Latitude and Longitude.  If Lat=Lon=0, then loiter at the current position.  Don't consider the navigation command complete (don't leave loiter) until the altitude has been reached.  Additionally, if the Heading Required parameter is non-zero the  aircraft will not leave the loiter until heading toward the next waypoint. ''')
enums['MAV_CMD'][31].param[1] = '''Heading Required (0 = False)'''
enums['MAV_CMD'][31].param[2] = '''Radius in meters. If positive loiter clockwise, negative counter-clockwise, 0 means no change to standard loiter.'''
enums['MAV_CMD'][31].param[3] = '''Empty'''
enums['MAV_CMD'][31].param[4] = '''Empty'''
enums['MAV_CMD'][31].param[5] = '''Latitude'''
enums['MAV_CMD'][31].param[6] = '''Longitude'''
enums['MAV_CMD'][31].param[7] = '''Altitude'''
MAV_CMD_NAV_ROI = 80 # Sets the region of interest (ROI) for a sensor set or the vehicle
                        # itself. This can then be used by the
                        # vehicles control system to control the
                        # vehicle attitude and the attitude of various
                        # sensors such as cameras.
enums['MAV_CMD'][80] = EnumEntry('MAV_CMD_NAV_ROI', '''Sets the region of interest (ROI) for a sensor set or the vehicle itself. This can then be used by the vehicles control system to control the vehicle attitude and the attitude of various sensors such as cameras.''')
enums['MAV_CMD'][80].param[1] = '''Region of intereset mode. (see MAV_ROI enum)'''
enums['MAV_CMD'][80].param[2] = '''MISSION index/ target ID. (see MAV_ROI enum)'''
enums['MAV_CMD'][80].param[3] = '''ROI index (allows a vehicle to manage multiple ROI's)'''
enums['MAV_CMD'][80].param[4] = '''Empty'''
enums['MAV_CMD'][80].param[5] = '''x the location of the fixed ROI (see MAV_FRAME)'''
enums['MAV_CMD'][80].param[6] = '''y'''
enums['MAV_CMD'][80].param[7] = '''z'''
MAV_CMD_NAV_PATHPLANNING = 81 # Control autonomous path planning on the MAV.
enums['MAV_CMD'][81] = EnumEntry('MAV_CMD_NAV_PATHPLANNING', '''Control autonomous path planning on the MAV.''')
enums['MAV_CMD'][81].param[1] = '''0: Disable local obstacle avoidance / local path planning (without resetting map), 1: Enable local path planning, 2: Enable and reset local path planning'''
enums['MAV_CMD'][81].param[2] = '''0: Disable full path planning (without resetting map), 1: Enable, 2: Enable and reset map/occupancy grid, 3: Enable and reset planned route, but not occupancy grid'''
enums['MAV_CMD'][81].param[3] = '''Empty'''
enums['MAV_CMD'][81].param[4] = '''Yaw angle at goal, in compass degrees, [0..360]'''
enums['MAV_CMD'][81].param[5] = '''Latitude/X of goal'''
enums['MAV_CMD'][81].param[6] = '''Longitude/Y of goal'''
enums['MAV_CMD'][81].param[7] = '''Altitude/Z of goal'''
MAV_CMD_NAV_SPLINE_WAYPOINT = 82 # Navigate to MISSION using a spline path.
enums['MAV_CMD'][82] = EnumEntry('MAV_CMD_NAV_SPLINE_WAYPOINT', '''Navigate to MISSION using a spline path.''')
enums['MAV_CMD'][82].param[1] = '''Hold time in decimal seconds. (ignored by fixed wing, time to stay at MISSION for rotary wing)'''
enums['MAV_CMD'][82].param[2] = '''Empty'''
enums['MAV_CMD'][82].param[3] = '''Empty'''
enums['MAV_CMD'][82].param[4] = '''Empty'''
enums['MAV_CMD'][82].param[5] = '''Latitude/X of goal'''
enums['MAV_CMD'][82].param[6] = '''Longitude/Y of goal'''
enums['MAV_CMD'][82].param[7] = '''Altitude/Z of goal'''
MAV_CMD_NAV_GUIDED_ENABLE = 92 # hand control over to an external controller
enums['MAV_CMD'][92] = EnumEntry('MAV_CMD_NAV_GUIDED_ENABLE', '''hand control over to an external controller''')
enums['MAV_CMD'][92].param[1] = '''On / Off (> 0.5f on)'''
enums['MAV_CMD'][92].param[2] = '''Empty'''
enums['MAV_CMD'][92].param[3] = '''Empty'''
enums['MAV_CMD'][92].param[4] = '''Empty'''
enums['MAV_CMD'][92].param[5] = '''Empty'''
enums['MAV_CMD'][92].param[6] = '''Empty'''
enums['MAV_CMD'][92].param[7] = '''Empty'''
MAV_CMD_NAV_LAST = 95 # NOP - This command is only used to mark the upper limit of the
                        # NAV/ACTION commands in the enumeration
enums['MAV_CMD'][95] = EnumEntry('MAV_CMD_NAV_LAST', '''NOP - This command is only used to mark the upper limit of the NAV/ACTION commands in the enumeration''')
enums['MAV_CMD'][95].param[1] = '''Empty'''
enums['MAV_CMD'][95].param[2] = '''Empty'''
enums['MAV_CMD'][95].param[3] = '''Empty'''
enums['MAV_CMD'][95].param[4] = '''Empty'''
enums['MAV_CMD'][95].param[5] = '''Empty'''
enums['MAV_CMD'][95].param[6] = '''Empty'''
enums['MAV_CMD'][95].param[7] = '''Empty'''
MAV_CMD_CONDITION_DELAY = 112 # Delay mission state machine.
enums['MAV_CMD'][112] = EnumEntry('MAV_CMD_CONDITION_DELAY', '''Delay mission state machine.''')
enums['MAV_CMD'][112].param[1] = '''Delay in seconds (decimal)'''
enums['MAV_CMD'][112].param[2] = '''Empty'''
enums['MAV_CMD'][112].param[3] = '''Empty'''
enums['MAV_CMD'][112].param[4] = '''Empty'''
enums['MAV_CMD'][112].param[5] = '''Empty'''
enums['MAV_CMD'][112].param[6] = '''Empty'''
enums['MAV_CMD'][112].param[7] = '''Empty'''
MAV_CMD_CONDITION_CHANGE_ALT = 113 # Ascend/descend at rate.  Delay mission state machine until desired
                        # altitude reached.
enums['MAV_CMD'][113] = EnumEntry('MAV_CMD_CONDITION_CHANGE_ALT', '''Ascend/descend at rate.  Delay mission state machine until desired altitude reached.''')
enums['MAV_CMD'][113].param[1] = '''Descent / Ascend rate (m/s)'''
enums['MAV_CMD'][113].param[2] = '''Empty'''
enums['MAV_CMD'][113].param[3] = '''Empty'''
enums['MAV_CMD'][113].param[4] = '''Empty'''
enums['MAV_CMD'][113].param[5] = '''Empty'''
enums['MAV_CMD'][113].param[6] = '''Empty'''
enums['MAV_CMD'][113].param[7] = '''Finish Altitude'''
MAV_CMD_CONDITION_DISTANCE = 114 # Delay mission state machine until within desired distance of next NAV
                        # point.
enums['MAV_CMD'][114] = EnumEntry('MAV_CMD_CONDITION_DISTANCE', '''Delay mission state machine until within desired distance of next NAV point.''')
enums['MAV_CMD'][114].param[1] = '''Distance (meters)'''
enums['MAV_CMD'][114].param[2] = '''Empty'''
enums['MAV_CMD'][114].param[3] = '''Empty'''
enums['MAV_CMD'][114].param[4] = '''Empty'''
enums['MAV_CMD'][114].param[5] = '''Empty'''
enums['MAV_CMD'][114].param[6] = '''Empty'''
enums['MAV_CMD'][114].param[7] = '''Empty'''
MAV_CMD_CONDITION_YAW = 115 # Reach a certain target angle.
enums['MAV_CMD'][115] = EnumEntry('MAV_CMD_CONDITION_YAW', '''Reach a certain target angle.''')
enums['MAV_CMD'][115].param[1] = '''target angle: [0-360], 0 is north'''
enums['MAV_CMD'][115].param[2] = '''speed during yaw change:[deg per second]'''
enums['MAV_CMD'][115].param[3] = '''direction: negative: counter clockwise, positive: clockwise [-1,1]'''
enums['MAV_CMD'][115].param[4] = '''relative offset or absolute angle: [ 1,0]'''
enums['MAV_CMD'][115].param[5] = '''Empty'''
enums['MAV_CMD'][115].param[6] = '''Empty'''
enums['MAV_CMD'][115].param[7] = '''Empty'''
MAV_CMD_CONDITION_LAST = 159 # NOP - This command is only used to mark the upper limit of the
                        # CONDITION commands in the enumeration
enums['MAV_CMD'][159] = EnumEntry('MAV_CMD_CONDITION_LAST', '''NOP - This command is only used to mark the upper limit of the CONDITION commands in the enumeration''')
enums['MAV_CMD'][159].param[1] = '''Empty'''
enums['MAV_CMD'][159].param[2] = '''Empty'''
enums['MAV_CMD'][159].param[3] = '''Empty'''
enums['MAV_CMD'][159].param[4] = '''Empty'''
enums['MAV_CMD'][159].param[5] = '''Empty'''
enums['MAV_CMD'][159].param[6] = '''Empty'''
enums['MAV_CMD'][159].param[7] = '''Empty'''
MAV_CMD_DO_SET_MODE = 176 # Set system mode.
enums['MAV_CMD'][176] = EnumEntry('MAV_CMD_DO_SET_MODE', '''Set system mode.''')
enums['MAV_CMD'][176].param[1] = '''Mode, as defined by ENUM MAV_MODE'''
enums['MAV_CMD'][176].param[2] = '''Custom mode - this is system specific, please refer to the individual autopilot specifications for details.'''
enums['MAV_CMD'][176].param[3] = '''Empty'''
enums['MAV_CMD'][176].param[4] = '''Empty'''
enums['MAV_CMD'][176].param[5] = '''Empty'''
enums['MAV_CMD'][176].param[6] = '''Empty'''
enums['MAV_CMD'][176].param[7] = '''Empty'''
MAV_CMD_DO_JUMP = 177 # Jump to the desired command in the mission list.  Repeat this action
                        # only the specified number of times
enums['MAV_CMD'][177] = EnumEntry('MAV_CMD_DO_JUMP', '''Jump to the desired command in the mission list.  Repeat this action only the specified number of times''')
enums['MAV_CMD'][177].param[1] = '''Sequence number'''
enums['MAV_CMD'][177].param[2] = '''Repeat count'''
enums['MAV_CMD'][177].param[3] = '''Empty'''
enums['MAV_CMD'][177].param[4] = '''Empty'''
enums['MAV_CMD'][177].param[5] = '''Empty'''
enums['MAV_CMD'][177].param[6] = '''Empty'''
enums['MAV_CMD'][177].param[7] = '''Empty'''
MAV_CMD_DO_CHANGE_SPEED = 178 # Change speed and/or throttle set points.
enums['MAV_CMD'][178] = EnumEntry('MAV_CMD_DO_CHANGE_SPEED', '''Change speed and/or throttle set points.''')
enums['MAV_CMD'][178].param[1] = '''Speed type (0=Airspeed, 1=Ground Speed)'''
enums['MAV_CMD'][178].param[2] = '''Speed  (m/s, -1 indicates no change)'''
enums['MAV_CMD'][178].param[3] = '''Throttle  ( Percent, -1 indicates no change)'''
enums['MAV_CMD'][178].param[4] = '''Empty'''
enums['MAV_CMD'][178].param[5] = '''Empty'''
enums['MAV_CMD'][178].param[6] = '''Empty'''
enums['MAV_CMD'][178].param[7] = '''Empty'''
MAV_CMD_DO_SET_HOME = 179 # Changes the home location either to the current location or a
                        # specified location.
enums['MAV_CMD'][179] = EnumEntry('MAV_CMD_DO_SET_HOME', '''Changes the home location either to the current location or a specified location.''')
enums['MAV_CMD'][179].param[1] = '''Use current (1=use current location, 0=use specified location)'''
enums['MAV_CMD'][179].param[2] = '''Empty'''
enums['MAV_CMD'][179].param[3] = '''Empty'''
enums['MAV_CMD'][179].param[4] = '''Empty'''
enums['MAV_CMD'][179].param[5] = '''Latitude'''
enums['MAV_CMD'][179].param[6] = '''Longitude'''
enums['MAV_CMD'][179].param[7] = '''Altitude'''
MAV_CMD_DO_SET_PARAMETER = 180 # Set a system parameter.  Caution!  Use of this command requires
                        # knowledge of the numeric enumeration value
                        # of the parameter.
enums['MAV_CMD'][180] = EnumEntry('MAV_CMD_DO_SET_PARAMETER', '''Set a system parameter.  Caution!  Use of this command requires knowledge of the numeric enumeration value of the parameter.''')
enums['MAV_CMD'][180].param[1] = '''Parameter number'''
enums['MAV_CMD'][180].param[2] = '''Parameter value'''
enums['MAV_CMD'][180].param[3] = '''Empty'''
enums['MAV_CMD'][180].param[4] = '''Empty'''
enums['MAV_CMD'][180].param[5] = '''Empty'''
enums['MAV_CMD'][180].param[6] = '''Empty'''
enums['MAV_CMD'][180].param[7] = '''Empty'''
MAV_CMD_DO_SET_RELAY = 181 # Set a relay to a condition.
enums['MAV_CMD'][181] = EnumEntry('MAV_CMD_DO_SET_RELAY', '''Set a relay to a condition.''')
enums['MAV_CMD'][181].param[1] = '''Relay number'''
enums['MAV_CMD'][181].param[2] = '''Setting (1=on, 0=off, others possible depending on system hardware)'''
enums['MAV_CMD'][181].param[3] = '''Empty'''
enums['MAV_CMD'][181].param[4] = '''Empty'''
enums['MAV_CMD'][181].param[5] = '''Empty'''
enums['MAV_CMD'][181].param[6] = '''Empty'''
enums['MAV_CMD'][181].param[7] = '''Empty'''
MAV_CMD_DO_REPEAT_RELAY = 182 # Cycle a relay on and off for a desired number of cyles with a desired
                        # period.
enums['MAV_CMD'][182] = EnumEntry('MAV_CMD_DO_REPEAT_RELAY', '''Cycle a relay on and off for a desired number of cyles with a desired period.''')
enums['MAV_CMD'][182].param[1] = '''Relay number'''
enums['MAV_CMD'][182].param[2] = '''Cycle count'''
enums['MAV_CMD'][182].param[3] = '''Cycle time (seconds, decimal)'''
enums['MAV_CMD'][182].param[4] = '''Empty'''
enums['MAV_CMD'][182].param[5] = '''Empty'''
enums['MAV_CMD'][182].param[6] = '''Empty'''
enums['MAV_CMD'][182].param[7] = '''Empty'''
MAV_CMD_DO_SET_SERVO = 183 # Set a servo to a desired PWM value.
enums['MAV_CMD'][183] = EnumEntry('MAV_CMD_DO_SET_SERVO', '''Set a servo to a desired PWM value.''')
enums['MAV_CMD'][183].param[1] = '''Servo number'''
enums['MAV_CMD'][183].param[2] = '''PWM (microseconds, 1000 to 2000 typical)'''
enums['MAV_CMD'][183].param[3] = '''Empty'''
enums['MAV_CMD'][183].param[4] = '''Empty'''
enums['MAV_CMD'][183].param[5] = '''Empty'''
enums['MAV_CMD'][183].param[6] = '''Empty'''
enums['MAV_CMD'][183].param[7] = '''Empty'''
MAV_CMD_DO_REPEAT_SERVO = 184 # Cycle a between its nominal setting and a desired PWM for a desired
                        # number of cycles with a desired period.
enums['MAV_CMD'][184] = EnumEntry('MAV_CMD_DO_REPEAT_SERVO', '''Cycle a between its nominal setting and a desired PWM for a desired number of cycles with a desired period.''')
enums['MAV_CMD'][184].param[1] = '''Servo number'''
enums['MAV_CMD'][184].param[2] = '''PWM (microseconds, 1000 to 2000 typical)'''
enums['MAV_CMD'][184].param[3] = '''Cycle count'''
enums['MAV_CMD'][184].param[4] = '''Cycle time (seconds)'''
enums['MAV_CMD'][184].param[5] = '''Empty'''
enums['MAV_CMD'][184].param[6] = '''Empty'''
enums['MAV_CMD'][184].param[7] = '''Empty'''
MAV_CMD_DO_FLIGHTTERMINATION = 185 # Terminate flight immediately
enums['MAV_CMD'][185] = EnumEntry('MAV_CMD_DO_FLIGHTTERMINATION', '''Terminate flight immediately''')
enums['MAV_CMD'][185].param[1] = '''Flight termination activated if > 0.5'''
enums['MAV_CMD'][185].param[2] = '''Empty'''
enums['MAV_CMD'][185].param[3] = '''Empty'''
enums['MAV_CMD'][185].param[4] = '''Empty'''
enums['MAV_CMD'][185].param[5] = '''Empty'''
enums['MAV_CMD'][185].param[6] = '''Empty'''
enums['MAV_CMD'][185].param[7] = '''Empty'''
MAV_CMD_DO_LAND_START = 189 # Mission command to perform a landing. This is used as a marker in a
                        # mission to tell the autopilot where a
                        # sequence of mission items that represents a
                        # landing starts. It may also be sent via a
                        # COMMAND_LONG to trigger a landing, in which
                        # case the nearest (geographically) landing
                        # sequence in the mission will be used. The
                        # Latitude/Longitude is optional, and may be
                        # set to 0/0 if not needed. If specified then
                        # it will be used to help find the closest
                        # landing sequence.
enums['MAV_CMD'][189] = EnumEntry('MAV_CMD_DO_LAND_START', '''Mission command to perform a landing. This is used as a marker in a mission to tell the autopilot where a sequence of mission items that represents a landing starts. It may also be sent via a COMMAND_LONG to trigger a landing, in which case the nearest (geographically) landing sequence in the mission will be used. The Latitude/Longitude is optional, and may be set to 0/0 if not needed. If specified then it will be used to help find the closest landing sequence.''')
enums['MAV_CMD'][189].param[1] = '''Empty'''
enums['MAV_CMD'][189].param[2] = '''Empty'''
enums['MAV_CMD'][189].param[3] = '''Empty'''
enums['MAV_CMD'][189].param[4] = '''Empty'''
enums['MAV_CMD'][189].param[5] = '''Latitude'''
enums['MAV_CMD'][189].param[6] = '''Longitude'''
enums['MAV_CMD'][189].param[7] = '''Empty'''
MAV_CMD_DO_RALLY_LAND = 190 # Mission command to perform a landing from a rally point.
enums['MAV_CMD'][190] = EnumEntry('MAV_CMD_DO_RALLY_LAND', '''Mission command to perform a landing from a rally point.''')
enums['MAV_CMD'][190].param[1] = '''Break altitude (meters)'''
enums['MAV_CMD'][190].param[2] = '''Landing speed (m/s)'''
enums['MAV_CMD'][190].param[3] = '''Empty'''
enums['MAV_CMD'][190].param[4] = '''Empty'''
enums['MAV_CMD'][190].param[5] = '''Empty'''
enums['MAV_CMD'][190].param[6] = '''Empty'''
enums['MAV_CMD'][190].param[7] = '''Empty'''
MAV_CMD_DO_GO_AROUND = 191 # Mission command to safely abort an autonmous landing.
enums['MAV_CMD'][191] = EnumEntry('MAV_CMD_DO_GO_AROUND', '''Mission command to safely abort an autonmous landing.''')
enums['MAV_CMD'][191].param[1] = '''Altitude (meters)'''
enums['MAV_CMD'][191].param[2] = '''Empty'''
enums['MAV_CMD'][191].param[3] = '''Empty'''
enums['MAV_CMD'][191].param[4] = '''Empty'''
enums['MAV_CMD'][191].param[5] = '''Empty'''
enums['MAV_CMD'][191].param[6] = '''Empty'''
enums['MAV_CMD'][191].param[7] = '''Empty'''
MAV_CMD_DO_CONTROL_VIDEO = 200 # Control onboard camera system.
enums['MAV_CMD'][200] = EnumEntry('MAV_CMD_DO_CONTROL_VIDEO', '''Control onboard camera system.''')
enums['MAV_CMD'][200].param[1] = '''Camera ID (-1 for all)'''
enums['MAV_CMD'][200].param[2] = '''Transmission: 0: disabled, 1: enabled compressed, 2: enabled raw'''
enums['MAV_CMD'][200].param[3] = '''Transmission mode: 0: video stream, >0: single images every n seconds (decimal)'''
enums['MAV_CMD'][200].param[4] = '''Recording: 0: disabled, 1: enabled compressed, 2: enabled raw'''
enums['MAV_CMD'][200].param[5] = '''Empty'''
enums['MAV_CMD'][200].param[6] = '''Empty'''
enums['MAV_CMD'][200].param[7] = '''Empty'''
MAV_CMD_DO_SET_ROI = 201 # Sets the region of interest (ROI) for a sensor set or the vehicle
                        # itself. This can then be used by the
                        # vehicles control system to control the
                        # vehicle attitude and the attitude of various
                        # sensors such as cameras.
enums['MAV_CMD'][201] = EnumEntry('MAV_CMD_DO_SET_ROI', '''Sets the region of interest (ROI) for a sensor set or the vehicle itself. This can then be used by the vehicles control system to control the vehicle attitude and the attitude of various sensors such as cameras.''')
enums['MAV_CMD'][201].param[1] = '''Region of intereset mode. (see MAV_ROI enum)'''
enums['MAV_CMD'][201].param[2] = '''MISSION index/ target ID. (see MAV_ROI enum)'''
enums['MAV_CMD'][201].param[3] = '''ROI index (allows a vehicle to manage multiple ROI's)'''
enums['MAV_CMD'][201].param[4] = '''Empty'''
enums['MAV_CMD'][201].param[5] = '''x the location of the fixed ROI (see MAV_FRAME)'''
enums['MAV_CMD'][201].param[6] = '''y'''
enums['MAV_CMD'][201].param[7] = '''z'''
MAV_CMD_DO_DIGICAM_CONFIGURE = 202 # Mission command to configure an on-board camera controller system.
enums['MAV_CMD'][202] = EnumEntry('MAV_CMD_DO_DIGICAM_CONFIGURE', '''Mission command to configure an on-board camera controller system.''')
enums['MAV_CMD'][202].param[1] = '''Modes: P, TV, AV, M, Etc'''
enums['MAV_CMD'][202].param[2] = '''Shutter speed: Divisor number for one second'''
enums['MAV_CMD'][202].param[3] = '''Aperture: F stop number'''
enums['MAV_CMD'][202].param[4] = '''ISO number e.g. 80, 100, 200, Etc'''
enums['MAV_CMD'][202].param[5] = '''Exposure type enumerator'''
enums['MAV_CMD'][202].param[6] = '''Command Identity'''
enums['MAV_CMD'][202].param[7] = '''Main engine cut-off time before camera trigger in seconds/10 (0 means no cut-off)'''
MAV_CMD_DO_DIGICAM_CONTROL = 203 # Mission command to control an on-board camera controller system.
enums['MAV_CMD'][203] = EnumEntry('MAV_CMD_DO_DIGICAM_CONTROL', '''Mission command to control an on-board camera controller system.''')
enums['MAV_CMD'][203].param[1] = '''Session control e.g. show/hide lens'''
enums['MAV_CMD'][203].param[2] = '''Zoom's absolute position'''
enums['MAV_CMD'][203].param[3] = '''Zooming step value to offset zoom from the current position'''
enums['MAV_CMD'][203].param[4] = '''Focus Locking, Unlocking or Re-locking'''
enums['MAV_CMD'][203].param[5] = '''Shooting Command'''
enums['MAV_CMD'][203].param[6] = '''Command Identity'''
enums['MAV_CMD'][203].param[7] = '''Empty'''
MAV_CMD_DO_MOUNT_CONFIGURE = 204 # Mission command to configure a camera or antenna mount
enums['MAV_CMD'][204] = EnumEntry('MAV_CMD_DO_MOUNT_CONFIGURE', '''Mission command to configure a camera or antenna mount''')
enums['MAV_CMD'][204].param[1] = '''Mount operation mode (see MAV_MOUNT_MODE enum)'''
enums['MAV_CMD'][204].param[2] = '''stabilize roll? (1 = yes, 0 = no)'''
enums['MAV_CMD'][204].param[3] = '''stabilize pitch? (1 = yes, 0 = no)'''
enums['MAV_CMD'][204].param[4] = '''stabilize yaw? (1 = yes, 0 = no)'''
enums['MAV_CMD'][204].param[5] = '''Empty'''
enums['MAV_CMD'][204].param[6] = '''Empty'''
enums['MAV_CMD'][204].param[7] = '''Empty'''
MAV_CMD_DO_MOUNT_CONTROL = 205 # Mission command to control a camera or antenna mount
enums['MAV_CMD'][205] = EnumEntry('MAV_CMD_DO_MOUNT_CONTROL', '''Mission command to control a camera or antenna mount''')
enums['MAV_CMD'][205].param[1] = '''pitch or lat in degrees, depending on mount mode.'''
enums['MAV_CMD'][205].param[2] = '''roll or lon in degrees depending on mount mode'''
enums['MAV_CMD'][205].param[3] = '''yaw or alt (in meters) depending on mount mode'''
enums['MAV_CMD'][205].param[4] = '''reserved'''
enums['MAV_CMD'][205].param[5] = '''reserved'''
enums['MAV_CMD'][205].param[6] = '''reserved'''
enums['MAV_CMD'][205].param[7] = '''MAV_MOUNT_MODE enum value'''
MAV_CMD_DO_SET_CAM_TRIGG_DIST = 206 # Mission command to set CAM_TRIGG_DIST for this flight
enums['MAV_CMD'][206] = EnumEntry('MAV_CMD_DO_SET_CAM_TRIGG_DIST', '''Mission command to set CAM_TRIGG_DIST for this flight''')
enums['MAV_CMD'][206].param[1] = '''Camera trigger distance (meters)'''
enums['MAV_CMD'][206].param[2] = '''Empty'''
enums['MAV_CMD'][206].param[3] = '''Empty'''
enums['MAV_CMD'][206].param[4] = '''Empty'''
enums['MAV_CMD'][206].param[5] = '''Empty'''
enums['MAV_CMD'][206].param[6] = '''Empty'''
enums['MAV_CMD'][206].param[7] = '''Empty'''
MAV_CMD_DO_FENCE_ENABLE = 207 # Mission command to enable the geofence
enums['MAV_CMD'][207] = EnumEntry('MAV_CMD_DO_FENCE_ENABLE', '''Mission command to enable the geofence''')
enums['MAV_CMD'][207].param[1] = '''enable? (0=disable, 1=enable)'''
enums['MAV_CMD'][207].param[2] = '''Empty'''
enums['MAV_CMD'][207].param[3] = '''Empty'''
enums['MAV_CMD'][207].param[4] = '''Empty'''
enums['MAV_CMD'][207].param[5] = '''Empty'''
enums['MAV_CMD'][207].param[6] = '''Empty'''
enums['MAV_CMD'][207].param[7] = '''Empty'''
MAV_CMD_DO_PARACHUTE = 208 # Mission command to trigger a parachute
enums['MAV_CMD'][208] = EnumEntry('MAV_CMD_DO_PARACHUTE', '''Mission command to trigger a parachute''')
enums['MAV_CMD'][208].param[1] = '''action (0=disable, 1=enable, 2=release, for some systems see PARACHUTE_ACTION enum, not in general message set.)'''
enums['MAV_CMD'][208].param[2] = '''Empty'''
enums['MAV_CMD'][208].param[3] = '''Empty'''
enums['MAV_CMD'][208].param[4] = '''Empty'''
enums['MAV_CMD'][208].param[5] = '''Empty'''
enums['MAV_CMD'][208].param[6] = '''Empty'''
enums['MAV_CMD'][208].param[7] = '''Empty'''
MAV_CMD_DO_INVERTED_FLIGHT = 210 # Change to/from inverted flight
enums['MAV_CMD'][210] = EnumEntry('MAV_CMD_DO_INVERTED_FLIGHT', '''Change to/from inverted flight''')
enums['MAV_CMD'][210].param[1] = '''inverted (0=normal, 1=inverted)'''
enums['MAV_CMD'][210].param[2] = '''Empty'''
enums['MAV_CMD'][210].param[3] = '''Empty'''
enums['MAV_CMD'][210].param[4] = '''Empty'''
enums['MAV_CMD'][210].param[5] = '''Empty'''
enums['MAV_CMD'][210].param[6] = '''Empty'''
enums['MAV_CMD'][210].param[7] = '''Empty'''
MAV_CMD_DO_MOUNT_CONTROL_QUAT = 220 # Mission command to control a camera or antenna mount, using a
                        # quaternion as reference.
enums['MAV_CMD'][220] = EnumEntry('MAV_CMD_DO_MOUNT_CONTROL_QUAT', '''Mission command to control a camera or antenna mount, using a quaternion as reference.''')
enums['MAV_CMD'][220].param[1] = '''q1 - quaternion param #1, w (1 in null-rotation)'''
enums['MAV_CMD'][220].param[2] = '''q2 - quaternion param #2, x (0 in null-rotation)'''
enums['MAV_CMD'][220].param[3] = '''q3 - quaternion param #3, y (0 in null-rotation)'''
enums['MAV_CMD'][220].param[4] = '''q4 - quaternion param #4, z (0 in null-rotation)'''
enums['MAV_CMD'][220].param[5] = '''Empty'''
enums['MAV_CMD'][220].param[6] = '''Empty'''
enums['MAV_CMD'][220].param[7] = '''Empty'''
MAV_CMD_DO_GUIDED_MASTER = 221 # set id of master controller
enums['MAV_CMD'][221] = EnumEntry('MAV_CMD_DO_GUIDED_MASTER', '''set id of master controller''')
enums['MAV_CMD'][221].param[1] = '''System ID'''
enums['MAV_CMD'][221].param[2] = '''Component ID'''
enums['MAV_CMD'][221].param[3] = '''Empty'''
enums['MAV_CMD'][221].param[4] = '''Empty'''
enums['MAV_CMD'][221].param[5] = '''Empty'''
enums['MAV_CMD'][221].param[6] = '''Empty'''
enums['MAV_CMD'][221].param[7] = '''Empty'''
MAV_CMD_DO_GUIDED_LIMITS = 222 # set limits for external control
enums['MAV_CMD'][222] = EnumEntry('MAV_CMD_DO_GUIDED_LIMITS', '''set limits for external control''')
enums['MAV_CMD'][222].param[1] = '''timeout - maximum time (in seconds) that external controller will be allowed to control vehicle. 0 means no timeout'''
enums['MAV_CMD'][222].param[2] = '''absolute altitude min (in meters, AMSL) - if vehicle moves below this alt, the command will be aborted and the mission will continue.  0 means no lower altitude limit'''
enums['MAV_CMD'][222].param[3] = '''absolute altitude max (in meters)- if vehicle moves above this alt, the command will be aborted and the mission will continue.  0 means no upper altitude limit'''
enums['MAV_CMD'][222].param[4] = '''horizontal move limit (in meters, AMSL) - if vehicle moves more than this distance from it's location at the moment the command was executed, the command will be aborted and the mission will continue. 0 means no horizontal altitude limit'''
enums['MAV_CMD'][222].param[5] = '''Empty'''
enums['MAV_CMD'][222].param[6] = '''Empty'''
enums['MAV_CMD'][222].param[7] = '''Empty'''
MAV_CMD_DO_LAST = 240 # NOP - This command is only used to mark the upper limit of the DO
                        # commands in the enumeration
enums['MAV_CMD'][240] = EnumEntry('MAV_CMD_DO_LAST', '''NOP - This command is only used to mark the upper limit of the DO commands in the enumeration''')
enums['MAV_CMD'][240].param[1] = '''Empty'''
enums['MAV_CMD'][240].param[2] = '''Empty'''
enums['MAV_CMD'][240].param[3] = '''Empty'''
enums['MAV_CMD'][240].param[4] = '''Empty'''
enums['MAV_CMD'][240].param[5] = '''Empty'''
enums['MAV_CMD'][240].param[6] = '''Empty'''
enums['MAV_CMD'][240].param[7] = '''Empty'''
MAV_CMD_PREFLIGHT_CALIBRATION = 241 # Trigger calibration. This command will be only accepted if in pre-
                        # flight mode.
enums['MAV_CMD'][241] = EnumEntry('MAV_CMD_PREFLIGHT_CALIBRATION', '''Trigger calibration. This command will be only accepted if in pre-flight mode.''')
enums['MAV_CMD'][241].param[1] = '''Gyro calibration: 0: no, 1: yes'''
enums['MAV_CMD'][241].param[2] = '''Magnetometer calibration: 0: no, 1: yes'''
enums['MAV_CMD'][241].param[3] = '''Ground pressure: 0: no, 1: yes'''
enums['MAV_CMD'][241].param[4] = '''Radio calibration: 0: no, 1: yes'''
enums['MAV_CMD'][241].param[5] = '''Accelerometer calibration: 0: no, 1: yes'''
enums['MAV_CMD'][241].param[6] = '''Compass/Motor interference calibration: 0: no, 1: yes'''
enums['MAV_CMD'][241].param[7] = '''Empty'''
MAV_CMD_PREFLIGHT_SET_SENSOR_OFFSETS = 242 # Set sensor offsets. This command will be only accepted if in pre-
                        # flight mode.
enums['MAV_CMD'][242] = EnumEntry('MAV_CMD_PREFLIGHT_SET_SENSOR_OFFSETS', '''Set sensor offsets. This command will be only accepted if in pre-flight mode.''')
enums['MAV_CMD'][242].param[1] = '''Sensor to adjust the offsets for: 0: gyros, 1: accelerometer, 2: magnetometer, 3: barometer, 4: optical flow, 5: second magnetometer'''
enums['MAV_CMD'][242].param[2] = '''X axis offset (or generic dimension 1), in the sensor's raw units'''
enums['MAV_CMD'][242].param[3] = '''Y axis offset (or generic dimension 2), in the sensor's raw units'''
enums['MAV_CMD'][242].param[4] = '''Z axis offset (or generic dimension 3), in the sensor's raw units'''
enums['MAV_CMD'][242].param[5] = '''Generic dimension 4, in the sensor's raw units'''
enums['MAV_CMD'][242].param[6] = '''Generic dimension 5, in the sensor's raw units'''
enums['MAV_CMD'][242].param[7] = '''Generic dimension 6, in the sensor's raw units'''
MAV_CMD_PREFLIGHT_STORAGE = 245 # Request storage of different parameter values and logs. This command
                        # will be only accepted if in pre-flight mode.
enums['MAV_CMD'][245] = EnumEntry('MAV_CMD_PREFLIGHT_STORAGE', '''Request storage of different parameter values and logs. This command will be only accepted if in pre-flight mode.''')
enums['MAV_CMD'][245].param[1] = '''Parameter storage: 0: READ FROM FLASH/EEPROM, 1: WRITE CURRENT TO FLASH/EEPROM'''
enums['MAV_CMD'][245].param[2] = '''Mission storage: 0: READ FROM FLASH/EEPROM, 1: WRITE CURRENT TO FLASH/EEPROM'''
enums['MAV_CMD'][245].param[3] = '''Onboard logging: 0: Ignore, 1: Start default rate logging, -1: Stop logging, > 1: start logging with rate of param 3 in Hz (e.g. set to 1000 for 1000 Hz logging)'''
enums['MAV_CMD'][245].param[4] = '''Reserved'''
enums['MAV_CMD'][245].param[5] = '''Empty'''
enums['MAV_CMD'][245].param[6] = '''Empty'''
enums['MAV_CMD'][245].param[7] = '''Empty'''
MAV_CMD_PREFLIGHT_REBOOT_SHUTDOWN = 246 # Request the reboot or shutdown of system components.
enums['MAV_CMD'][246] = EnumEntry('MAV_CMD_PREFLIGHT_REBOOT_SHUTDOWN', '''Request the reboot or shutdown of system components.''')
enums['MAV_CMD'][246].param[1] = '''0: Do nothing for autopilot, 1: Reboot autopilot, 2: Shutdown autopilot.'''
enums['MAV_CMD'][246].param[2] = '''0: Do nothing for onboard computer, 1: Reboot onboard computer, 2: Shutdown onboard computer.'''
enums['MAV_CMD'][246].param[3] = '''Reserved'''
enums['MAV_CMD'][246].param[4] = '''Reserved'''
enums['MAV_CMD'][246].param[5] = '''Empty'''
enums['MAV_CMD'][246].param[6] = '''Empty'''
enums['MAV_CMD'][246].param[7] = '''Empty'''
MAV_CMD_OVERRIDE_GOTO = 252 # Hold / continue the current action
enums['MAV_CMD'][252] = EnumEntry('MAV_CMD_OVERRIDE_GOTO', '''Hold / continue the current action''')
enums['MAV_CMD'][252].param[1] = '''MAV_GOTO_DO_HOLD: hold MAV_GOTO_DO_CONTINUE: continue with next item in mission plan'''
enums['MAV_CMD'][252].param[2] = '''MAV_GOTO_HOLD_AT_CURRENT_POSITION: Hold at current position MAV_GOTO_HOLD_AT_SPECIFIED_POSITION: hold at specified position'''
enums['MAV_CMD'][252].param[3] = '''MAV_FRAME coordinate frame of hold point'''
enums['MAV_CMD'][252].param[4] = '''Desired yaw angle in degrees'''
enums['MAV_CMD'][252].param[5] = '''Latitude / X position'''
enums['MAV_CMD'][252].param[6] = '''Longitude / Y position'''
enums['MAV_CMD'][252].param[7] = '''Altitude / Z position'''
MAV_CMD_MISSION_START = 300 # start running a mission
enums['MAV_CMD'][300] = EnumEntry('MAV_CMD_MISSION_START', '''start running a mission''')
enums['MAV_CMD'][300].param[1] = '''first_item: the first mission item to run'''
enums['MAV_CMD'][300].param[2] = '''last_item:  the last mission item to run (after this item is run, the mission ends)'''
MAV_CMD_COMPONENT_ARM_DISARM = 400 # Arms / Disarms a component
enums['MAV_CMD'][400] = EnumEntry('MAV_CMD_COMPONENT_ARM_DISARM', '''Arms / Disarms a component''')
enums['MAV_CMD'][400].param[1] = '''1 to arm, 0 to disarm'''
MAV_CMD_START_RX_PAIR = 500 # Starts receiver pairing
enums['MAV_CMD'][500] = EnumEntry('MAV_CMD_START_RX_PAIR', '''Starts receiver pairing''')
enums['MAV_CMD'][500].param[1] = '''0:Spektrum'''
enums['MAV_CMD'][500].param[2] = '''0:Spektrum DSM2, 1:Spektrum DSMX'''
MAV_CMD_REQUEST_AUTOPILOT_CAPABILITIES = 520 # Request autopilot capabilities
enums['MAV_CMD'][520] = EnumEntry('MAV_CMD_REQUEST_AUTOPILOT_CAPABILITIES', '''Request autopilot capabilities''')
enums['MAV_CMD'][520].param[1] = '''1: Request autopilot version'''
enums['MAV_CMD'][520].param[2] = '''Reserved (all remaining params)'''
MAV_CMD_IMAGE_START_CAPTURE = 2000 # Start image capture sequence
enums['MAV_CMD'][2000] = EnumEntry('MAV_CMD_IMAGE_START_CAPTURE', '''Start image capture sequence''')
enums['MAV_CMD'][2000].param[1] = '''Duration between two consecutive pictures (in seconds)'''
enums['MAV_CMD'][2000].param[2] = '''Number of images to capture total - 0 for unlimited capture'''
enums['MAV_CMD'][2000].param[3] = '''Resolution in megapixels (0.3 for 640x480, 1.3 for 1280x720, etc)'''
MAV_CMD_IMAGE_STOP_CAPTURE = 2001 # Stop image capture sequence
enums['MAV_CMD'][2001] = EnumEntry('MAV_CMD_IMAGE_STOP_CAPTURE', '''Stop image capture sequence''')
enums['MAV_CMD'][2001].param[1] = '''Reserved'''
enums['MAV_CMD'][2001].param[2] = '''Reserved'''
MAV_CMD_DO_TRIGGER_CONTROL = 2003 # Enable or disable on-board camera triggering system.
enums['MAV_CMD'][2003] = EnumEntry('MAV_CMD_DO_TRIGGER_CONTROL', '''Enable or disable on-board camera triggering system.''')
enums['MAV_CMD'][2003].param[1] = '''Trigger enable/disable (0 for disable, 1 for start)'''
enums['MAV_CMD'][2003].param[2] = '''Shutter integration time (in ms)'''
enums['MAV_CMD'][2003].param[3] = '''Reserved'''
MAV_CMD_VIDEO_START_CAPTURE = 2500 # Starts video capture
enums['MAV_CMD'][2500] = EnumEntry('MAV_CMD_VIDEO_START_CAPTURE', '''Starts video capture''')
enums['MAV_CMD'][2500].param[1] = '''Camera ID (0 for all cameras), 1 for first, 2 for second, etc.'''
enums['MAV_CMD'][2500].param[2] = '''Frames per second'''
enums['MAV_CMD'][2500].param[3] = '''Resolution in megapixels (0.3 for 640x480, 1.3 for 1280x720, etc)'''
MAV_CMD_VIDEO_STOP_CAPTURE = 2501 # Stop the current video capture
enums['MAV_CMD'][2501] = EnumEntry('MAV_CMD_VIDEO_STOP_CAPTURE', '''Stop the current video capture''')
enums['MAV_CMD'][2501].param[1] = '''Reserved'''
enums['MAV_CMD'][2501].param[2] = '''Reserved'''
MAV_CMD_PANORAMA_CREATE = 2800 # Create a panorama at the current position
enums['MAV_CMD'][2800] = EnumEntry('MAV_CMD_PANORAMA_CREATE', '''Create a panorama at the current position''')
enums['MAV_CMD'][2800].param[1] = '''Viewing angle horizontal of the panorama (in degrees, +- 0.5 the total angle)'''
enums['MAV_CMD'][2800].param[2] = '''Viewing angle vertical of panorama (in degrees)'''
enums['MAV_CMD'][2800].param[3] = '''Speed of the horizontal rotation (in degrees per second)'''
enums['MAV_CMD'][2800].param[4] = '''Speed of the vertical rotation (in degrees per second)'''
MAV_CMD_PAYLOAD_PREPARE_DEPLOY = 30001 # Deploy payload on a Lat / Lon / Alt position. This includes the
                        # navigation to reach the required release
                        # position and velocity.
enums['MAV_CMD'][30001] = EnumEntry('MAV_CMD_PAYLOAD_PREPARE_DEPLOY', '''Deploy payload on a Lat / Lon / Alt position. This includes the navigation to reach the required release position and velocity.''')
enums['MAV_CMD'][30001].param[1] = '''Operation mode. 0: prepare single payload deploy (overwriting previous requests), but do not execute it. 1: execute payload deploy immediately (rejecting further deploy commands during execution, but allowing abort). 2: add payload deploy to existing deployment list.'''
enums['MAV_CMD'][30001].param[2] = '''Desired approach vector in degrees compass heading (0..360). A negative value indicates the system can define the approach vector at will.'''
enums['MAV_CMD'][30001].param[3] = '''Desired ground speed at release time. This can be overriden by the airframe in case it needs to meet minimum airspeed. A negative value indicates the system can define the ground speed at will.'''
enums['MAV_CMD'][30001].param[4] = '''Minimum altitude clearance to the release position in meters. A negative value indicates the system can define the clearance at will.'''
enums['MAV_CMD'][30001].param[5] = '''Latitude unscaled for MISSION_ITEM or in 1e7 degrees for MISSION_ITEM_INT'''
enums['MAV_CMD'][30001].param[6] = '''Longitude unscaled for MISSION_ITEM or in 1e7 degrees for MISSION_ITEM_INT'''
enums['MAV_CMD'][30001].param[7] = '''Altitude, in meters AMSL'''
MAV_CMD_PAYLOAD_CONTROL_DEPLOY = 30002 # Control the payload deployment.
enums['MAV_CMD'][30002] = EnumEntry('MAV_CMD_PAYLOAD_CONTROL_DEPLOY', '''Control the payload deployment.''')
enums['MAV_CMD'][30002].param[1] = '''Operation mode. 0: Abort deployment, continue normal mission. 1: switch to payload deploment mode. 100: delete first payload deployment request. 101: delete all payload deployment requests.'''
enums['MAV_CMD'][30002].param[2] = '''Reserved'''
enums['MAV_CMD'][30002].param[3] = '''Reserved'''
enums['MAV_CMD'][30002].param[4] = '''Reserved'''
enums['MAV_CMD'][30002].param[5] = '''Reserved'''
enums['MAV_CMD'][30002].param[6] = '''Reserved'''
enums['MAV_CMD'][30002].param[7] = '''Reserved'''
MAV_CMD_ENUM_END = 30003 # 
enums['MAV_CMD'][30003] = EnumEntry('MAV_CMD_ENUM_END', '''''')

# MAV_DATA_STREAM
enums['MAV_DATA_STREAM'] = {}
MAV_DATA_STREAM_ALL = 0 # Enable all data streams
enums['MAV_DATA_STREAM'][0] = EnumEntry('MAV_DATA_STREAM_ALL', '''Enable all data streams''')
MAV_DATA_STREAM_RAW_SENSORS = 1 # Enable IMU_RAW, GPS_RAW, GPS_STATUS packets.
enums['MAV_DATA_STREAM'][1] = EnumEntry('MAV_DATA_STREAM_RAW_SENSORS', '''Enable IMU_RAW, GPS_RAW, GPS_STATUS packets.''')
MAV_DATA_STREAM_EXTENDED_STATUS = 2 # Enable GPS_STATUS, CONTROL_STATUS, AUX_STATUS
enums['MAV_DATA_STREAM'][2] = EnumEntry('MAV_DATA_STREAM_EXTENDED_STATUS', '''Enable GPS_STATUS, CONTROL_STATUS, AUX_STATUS''')
MAV_DATA_STREAM_RC_CHANNELS = 3 # Enable RC_CHANNELS_SCALED, RC_CHANNELS_RAW, SERVO_OUTPUT_RAW
enums['MAV_DATA_STREAM'][3] = EnumEntry('MAV_DATA_STREAM_RC_CHANNELS', '''Enable RC_CHANNELS_SCALED, RC_CHANNELS_RAW, SERVO_OUTPUT_RAW''')
MAV_DATA_STREAM_RAW_CONTROLLER = 4 # Enable ATTITUDE_CONTROLLER_OUTPUT, POSITION_CONTROLLER_OUTPUT,
                        # NAV_CONTROLLER_OUTPUT.
enums['MAV_DATA_STREAM'][4] = EnumEntry('MAV_DATA_STREAM_RAW_CONTROLLER', '''Enable ATTITUDE_CONTROLLER_OUTPUT, POSITION_CONTROLLER_OUTPUT, NAV_CONTROLLER_OUTPUT.''')
MAV_DATA_STREAM_POSITION = 6 # Enable LOCAL_POSITION, GLOBAL_POSITION/GLOBAL_POSITION_INT messages.
enums['MAV_DATA_STREAM'][6] = EnumEntry('MAV_DATA_STREAM_POSITION', '''Enable LOCAL_POSITION, GLOBAL_POSITION/GLOBAL_POSITION_INT messages.''')
MAV_DATA_STREAM_EXTRA1 = 10 # Dependent on the autopilot
enums['MAV_DATA_STREAM'][10] = EnumEntry('MAV_DATA_STREAM_EXTRA1', '''Dependent on the autopilot''')
MAV_DATA_STREAM_EXTRA2 = 11 # Dependent on the autopilot
enums['MAV_DATA_STREAM'][11] = EnumEntry('MAV_DATA_STREAM_EXTRA2', '''Dependent on the autopilot''')
MAV_DATA_STREAM_EXTRA3 = 12 # Dependent on the autopilot
enums['MAV_DATA_STREAM'][12] = EnumEntry('MAV_DATA_STREAM_EXTRA3', '''Dependent on the autopilot''')
MAV_DATA_STREAM_ENUM_END = 13 # 
enums['MAV_DATA_STREAM'][13] = EnumEntry('MAV_DATA_STREAM_ENUM_END', '''''')

# MAV_ROI
enums['MAV_ROI'] = {}
MAV_ROI_NONE = 0 # No region of interest.
enums['MAV_ROI'][0] = EnumEntry('MAV_ROI_NONE', '''No region of interest.''')
MAV_ROI_WPNEXT = 1 # Point toward next MISSION.
enums['MAV_ROI'][1] = EnumEntry('MAV_ROI_WPNEXT', '''Point toward next MISSION.''')
MAV_ROI_WPINDEX = 2 # Point toward given MISSION.
enums['MAV_ROI'][2] = EnumEntry('MAV_ROI_WPINDEX', '''Point toward given MISSION.''')
MAV_ROI_LOCATION = 3 # Point toward fixed location.
enums['MAV_ROI'][3] = EnumEntry('MAV_ROI_LOCATION', '''Point toward fixed location.''')
MAV_ROI_TARGET = 4 # Point toward of given id.
enums['MAV_ROI'][4] = EnumEntry('MAV_ROI_TARGET', '''Point toward of given id.''')
MAV_ROI_ENUM_END = 5 # 
enums['MAV_ROI'][5] = EnumEntry('MAV_ROI_ENUM_END', '''''')

# MAV_CMD_ACK
enums['MAV_CMD_ACK'] = {}
MAV_CMD_ACK_OK = 1 # Command / mission item is ok.
enums['MAV_CMD_ACK'][1] = EnumEntry('MAV_CMD_ACK_OK', '''Command / mission item is ok.''')
MAV_CMD_ACK_ERR_FAIL = 2 # Generic error message if none of the other reasons fails or if no
                        # detailed error reporting is implemented.
enums['MAV_CMD_ACK'][2] = EnumEntry('MAV_CMD_ACK_ERR_FAIL', '''Generic error message if none of the other reasons fails or if no detailed error reporting is implemented.''')
MAV_CMD_ACK_ERR_ACCESS_DENIED = 3 # The system is refusing to accept this command from this source /
                        # communication partner.
enums['MAV_CMD_ACK'][3] = EnumEntry('MAV_CMD_ACK_ERR_ACCESS_DENIED', '''The system is refusing to accept this command from this source / communication partner.''')
MAV_CMD_ACK_ERR_NOT_SUPPORTED = 4 # Command or mission item is not supported, other commands would be
                        # accepted.
enums['MAV_CMD_ACK'][4] = EnumEntry('MAV_CMD_ACK_ERR_NOT_SUPPORTED', '''Command or mission item is not supported, other commands would be accepted.''')
MAV_CMD_ACK_ERR_COORDINATE_FRAME_NOT_SUPPORTED = 5 # The coordinate frame of this command / mission item is not supported.
enums['MAV_CMD_ACK'][5] = EnumEntry('MAV_CMD_ACK_ERR_COORDINATE_FRAME_NOT_SUPPORTED', '''The coordinate frame of this command / mission item is not supported.''')
MAV_CMD_ACK_ERR_COORDINATES_OUT_OF_RANGE = 6 # The coordinate frame of this command is ok, but he coordinate values
                        # exceed the safety limits of this system.
                        # This is a generic error, please use the more
                        # specific error messages below if possible.
enums['MAV_CMD_ACK'][6] = EnumEntry('MAV_CMD_ACK_ERR_COORDINATES_OUT_OF_RANGE', '''The coordinate frame of this command is ok, but he coordinate values exceed the safety limits of this system. This is a generic error, please use the more specific error messages below if possible.''')
MAV_CMD_ACK_ERR_X_LAT_OUT_OF_RANGE = 7 # The X or latitude value is out of range.
enums['MAV_CMD_ACK'][7] = EnumEntry('MAV_CMD_ACK_ERR_X_LAT_OUT_OF_RANGE', '''The X or latitude value is out of range.''')
MAV_CMD_ACK_ERR_Y_LON_OUT_OF_RANGE = 8 # The Y or longitude value is out of range.
enums['MAV_CMD_ACK'][8] = EnumEntry('MAV_CMD_ACK_ERR_Y_LON_OUT_OF_RANGE', '''The Y or longitude value is out of range.''')
MAV_CMD_ACK_ERR_Z_ALT_OUT_OF_RANGE = 9 # The Z or altitude value is out of range.
enums['MAV_CMD_ACK'][9] = EnumEntry('MAV_CMD_ACK_ERR_Z_ALT_OUT_OF_RANGE', '''The Z or altitude value is out of range.''')
MAV_CMD_ACK_ENUM_END = 10 # 
enums['MAV_CMD_ACK'][10] = EnumEntry('MAV_CMD_ACK_ENUM_END', '''''')

# MAV_PARAM_TYPE
enums['MAV_PARAM_TYPE'] = {}
MAV_PARAM_TYPE_UINT8 = 1 # 8-bit unsigned integer
enums['MAV_PARAM_TYPE'][1] = EnumEntry('MAV_PARAM_TYPE_UINT8', '''8-bit unsigned integer''')
MAV_PARAM_TYPE_INT8 = 2 # 8-bit signed integer
enums['MAV_PARAM_TYPE'][2] = EnumEntry('MAV_PARAM_TYPE_INT8', '''8-bit signed integer''')
MAV_PARAM_TYPE_UINT16 = 3 # 16-bit unsigned integer
enums['MAV_PARAM_TYPE'][3] = EnumEntry('MAV_PARAM_TYPE_UINT16', '''16-bit unsigned integer''')
MAV_PARAM_TYPE_INT16 = 4 # 16-bit signed integer
enums['MAV_PARAM_TYPE'][4] = EnumEntry('MAV_PARAM_TYPE_INT16', '''16-bit signed integer''')
MAV_PARAM_TYPE_UINT32 = 5 # 32-bit unsigned integer
enums['MAV_PARAM_TYPE'][5] = EnumEntry('MAV_PARAM_TYPE_UINT32', '''32-bit unsigned integer''')
MAV_PARAM_TYPE_INT32 = 6 # 32-bit signed integer
enums['MAV_PARAM_TYPE'][6] = EnumEntry('MAV_PARAM_TYPE_INT32', '''32-bit signed integer''')
MAV_PARAM_TYPE_UINT64 = 7 # 64-bit unsigned integer
enums['MAV_PARAM_TYPE'][7] = EnumEntry('MAV_PARAM_TYPE_UINT64', '''64-bit unsigned integer''')
MAV_PARAM_TYPE_INT64 = 8 # 64-bit signed integer
enums['MAV_PARAM_TYPE'][8] = EnumEntry('MAV_PARAM_TYPE_INT64', '''64-bit signed integer''')
MAV_PARAM_TYPE_REAL32 = 9 # 32-bit floating-point
enums['MAV_PARAM_TYPE'][9] = EnumEntry('MAV_PARAM_TYPE_REAL32', '''32-bit floating-point''')
MAV_PARAM_TYPE_REAL64 = 10 # 64-bit floating-point
enums['MAV_PARAM_TYPE'][10] = EnumEntry('MAV_PARAM_TYPE_REAL64', '''64-bit floating-point''')
MAV_PARAM_TYPE_ENUM_END = 11 # 
enums['MAV_PARAM_TYPE'][11] = EnumEntry('MAV_PARAM_TYPE_ENUM_END', '''''')

# MAV_RESULT
enums['MAV_RESULT'] = {}
MAV_RESULT_ACCEPTED = 0 # Command ACCEPTED and EXECUTED
enums['MAV_RESULT'][0] = EnumEntry('MAV_RESULT_ACCEPTED', '''Command ACCEPTED and EXECUTED''')
MAV_RESULT_TEMPORARILY_REJECTED = 1 # Command TEMPORARY REJECTED/DENIED
enums['MAV_RESULT'][1] = EnumEntry('MAV_RESULT_TEMPORARILY_REJECTED', '''Command TEMPORARY REJECTED/DENIED''')
MAV_RESULT_DENIED = 2 # Command PERMANENTLY DENIED
enums['MAV_RESULT'][2] = EnumEntry('MAV_RESULT_DENIED', '''Command PERMANENTLY DENIED''')
MAV_RESULT_UNSUPPORTED = 3 # Command UNKNOWN/UNSUPPORTED
enums['MAV_RESULT'][3] = EnumEntry('MAV_RESULT_UNSUPPORTED', '''Command UNKNOWN/UNSUPPORTED''')
MAV_RESULT_FAILED = 4 # Command executed, but failed
enums['MAV_RESULT'][4] = EnumEntry('MAV_RESULT_FAILED', '''Command executed, but failed''')
MAV_RESULT_ENUM_END = 5 # 
enums['MAV_RESULT'][5] = EnumEntry('MAV_RESULT_ENUM_END', '''''')

# MAV_MISSION_RESULT
enums['MAV_MISSION_RESULT'] = {}
MAV_MISSION_ACCEPTED = 0 # mission accepted OK
enums['MAV_MISSION_RESULT'][0] = EnumEntry('MAV_MISSION_ACCEPTED', '''mission accepted OK''')
MAV_MISSION_ERROR = 1 # generic error / not accepting mission commands at all right now
enums['MAV_MISSION_RESULT'][1] = EnumEntry('MAV_MISSION_ERROR', '''generic error / not accepting mission commands at all right now''')
MAV_MISSION_UNSUPPORTED_FRAME = 2 # coordinate frame is not supported
enums['MAV_MISSION_RESULT'][2] = EnumEntry('MAV_MISSION_UNSUPPORTED_FRAME', '''coordinate frame is not supported''')
MAV_MISSION_UNSUPPORTED = 3 # command is not supported
enums['MAV_MISSION_RESULT'][3] = EnumEntry('MAV_MISSION_UNSUPPORTED', '''command is not supported''')
MAV_MISSION_NO_SPACE = 4 # mission item exceeds storage space
enums['MAV_MISSION_RESULT'][4] = EnumEntry('MAV_MISSION_NO_SPACE', '''mission item exceeds storage space''')
MAV_MISSION_INVALID = 5 # one of the parameters has an invalid value
enums['MAV_MISSION_RESULT'][5] = EnumEntry('MAV_MISSION_INVALID', '''one of the parameters has an invalid value''')
MAV_MISSION_INVALID_PARAM1 = 6 # param1 has an invalid value
enums['MAV_MISSION_RESULT'][6] = EnumEntry('MAV_MISSION_INVALID_PARAM1', '''param1 has an invalid value''')
MAV_MISSION_INVALID_PARAM2 = 7 # param2 has an invalid value
enums['MAV_MISSION_RESULT'][7] = EnumEntry('MAV_MISSION_INVALID_PARAM2', '''param2 has an invalid value''')
MAV_MISSION_INVALID_PARAM3 = 8 # param3 has an invalid value
enums['MAV_MISSION_RESULT'][8] = EnumEntry('MAV_MISSION_INVALID_PARAM3', '''param3 has an invalid value''')
MAV_MISSION_INVALID_PARAM4 = 9 # param4 has an invalid value
enums['MAV_MISSION_RESULT'][9] = EnumEntry('MAV_MISSION_INVALID_PARAM4', '''param4 has an invalid value''')
MAV_MISSION_INVALID_PARAM5_X = 10 # x/param5 has an invalid value
enums['MAV_MISSION_RESULT'][10] = EnumEntry('MAV_MISSION_INVALID_PARAM5_X', '''x/param5 has an invalid value''')
MAV_MISSION_INVALID_PARAM6_Y = 11 # y/param6 has an invalid value
enums['MAV_MISSION_RESULT'][11] = EnumEntry('MAV_MISSION_INVALID_PARAM6_Y', '''y/param6 has an invalid value''')
MAV_MISSION_INVALID_PARAM7 = 12 # param7 has an invalid value
enums['MAV_MISSION_RESULT'][12] = EnumEntry('MAV_MISSION_INVALID_PARAM7', '''param7 has an invalid value''')
MAV_MISSION_INVALID_SEQUENCE = 13 # received waypoint out of sequence
enums['MAV_MISSION_RESULT'][13] = EnumEntry('MAV_MISSION_INVALID_SEQUENCE', '''received waypoint out of sequence''')
MAV_MISSION_DENIED = 14 # not accepting any mission commands from this communication partner
enums['MAV_MISSION_RESULT'][14] = EnumEntry('MAV_MISSION_DENIED', '''not accepting any mission commands from this communication partner''')
MAV_MISSION_RESULT_ENUM_END = 15 # 
enums['MAV_MISSION_RESULT'][15] = EnumEntry('MAV_MISSION_RESULT_ENUM_END', '''''')

# MAV_SEVERITY
enums['MAV_SEVERITY'] = {}
MAV_SEVERITY_EMERGENCY = 0 # System is unusable. This is a "panic" condition.
enums['MAV_SEVERITY'][0] = EnumEntry('MAV_SEVERITY_EMERGENCY', '''System is unusable. This is a "panic" condition.''')
MAV_SEVERITY_ALERT = 1 # Action should be taken immediately. Indicates error in non-critical
                        # systems.
enums['MAV_SEVERITY'][1] = EnumEntry('MAV_SEVERITY_ALERT', '''Action should be taken immediately. Indicates error in non-critical systems.''')
MAV_SEVERITY_CRITICAL = 2 # Action must be taken immediately. Indicates failure in a primary
                        # system.
enums['MAV_SEVERITY'][2] = EnumEntry('MAV_SEVERITY_CRITICAL', '''Action must be taken immediately. Indicates failure in a primary system.''')
MAV_SEVERITY_ERROR = 3 # Indicates an error in secondary/redundant systems.
enums['MAV_SEVERITY'][3] = EnumEntry('MAV_SEVERITY_ERROR', '''Indicates an error in secondary/redundant systems.''')
MAV_SEVERITY_WARNING = 4 # Indicates about a possible future error if this is not resolved within
                        # a given timeframe. Example would be a low
                        # battery warning.
enums['MAV_SEVERITY'][4] = EnumEntry('MAV_SEVERITY_WARNING', '''Indicates about a possible future error if this is not resolved within a given timeframe. Example would be a low battery warning.''')
MAV_SEVERITY_NOTICE = 5 # An unusual event has occured, though not an error condition. This
                        # should be investigated for the root cause.
enums['MAV_SEVERITY'][5] = EnumEntry('MAV_SEVERITY_NOTICE', '''An unusual event has occured, though not an error condition. This should be investigated for the root cause.''')
MAV_SEVERITY_INFO = 6 # Normal operational messages. Useful for logging. No action is required
                        # for these messages.
enums['MAV_SEVERITY'][6] = EnumEntry('MAV_SEVERITY_INFO', '''Normal operational messages. Useful for logging. No action is required for these messages.''')
MAV_SEVERITY_DEBUG = 7 # Useful non-operational messages that can assist in debugging. These
                        # should not occur during normal operation.
enums['MAV_SEVERITY'][7] = EnumEntry('MAV_SEVERITY_DEBUG', '''Useful non-operational messages that can assist in debugging. These should not occur during normal operation.''')
MAV_SEVERITY_ENUM_END = 8 # 
enums['MAV_SEVERITY'][8] = EnumEntry('MAV_SEVERITY_ENUM_END', '''''')

# MAV_POWER_STATUS
enums['MAV_POWER_STATUS'] = {}
MAV_POWER_STATUS_BRICK_VALID = 1 # main brick power supply valid
enums['MAV_POWER_STATUS'][1] = EnumEntry('MAV_POWER_STATUS_BRICK_VALID', '''main brick power supply valid''')
MAV_POWER_STATUS_SERVO_VALID = 2 # main servo power supply valid for FMU
enums['MAV_POWER_STATUS'][2] = EnumEntry('MAV_POWER_STATUS_SERVO_VALID', '''main servo power supply valid for FMU''')
MAV_POWER_STATUS_USB_CONNECTED = 4 # USB power is connected
enums['MAV_POWER_STATUS'][4] = EnumEntry('MAV_POWER_STATUS_USB_CONNECTED', '''USB power is connected''')
MAV_POWER_STATUS_PERIPH_OVERCURRENT = 8 # peripheral supply is in over-current state
enums['MAV_POWER_STATUS'][8] = EnumEntry('MAV_POWER_STATUS_PERIPH_OVERCURRENT', '''peripheral supply is in over-current state''')
MAV_POWER_STATUS_PERIPH_HIPOWER_OVERCURRENT = 16 # hi-power peripheral supply is in over-current state
enums['MAV_POWER_STATUS'][16] = EnumEntry('MAV_POWER_STATUS_PERIPH_HIPOWER_OVERCURRENT', '''hi-power peripheral supply is in over-current state''')
MAV_POWER_STATUS_CHANGED = 32 # Power status has changed since boot
enums['MAV_POWER_STATUS'][32] = EnumEntry('MAV_POWER_STATUS_CHANGED', '''Power status has changed since boot''')
MAV_POWER_STATUS_ENUM_END = 33 # 
enums['MAV_POWER_STATUS'][33] = EnumEntry('MAV_POWER_STATUS_ENUM_END', '''''')

# SERIAL_CONTROL_DEV
enums['SERIAL_CONTROL_DEV'] = {}
SERIAL_CONTROL_DEV_TELEM1 = 0 # First telemetry port
enums['SERIAL_CONTROL_DEV'][0] = EnumEntry('SERIAL_CONTROL_DEV_TELEM1', '''First telemetry port''')
SERIAL_CONTROL_DEV_TELEM2 = 1 # Second telemetry port
enums['SERIAL_CONTROL_DEV'][1] = EnumEntry('SERIAL_CONTROL_DEV_TELEM2', '''Second telemetry port''')
SERIAL_CONTROL_DEV_GPS1 = 2 # First GPS port
enums['SERIAL_CONTROL_DEV'][2] = EnumEntry('SERIAL_CONTROL_DEV_GPS1', '''First GPS port''')
SERIAL_CONTROL_DEV_GPS2 = 3 # Second GPS port
enums['SERIAL_CONTROL_DEV'][3] = EnumEntry('SERIAL_CONTROL_DEV_GPS2', '''Second GPS port''')
SERIAL_CONTROL_DEV_SHELL = 10 # system shell
enums['SERIAL_CONTROL_DEV'][10] = EnumEntry('SERIAL_CONTROL_DEV_SHELL', '''system shell''')
SERIAL_CONTROL_DEV_ENUM_END = 11 # 
enums['SERIAL_CONTROL_DEV'][11] = EnumEntry('SERIAL_CONTROL_DEV_ENUM_END', '''''')

# SERIAL_CONTROL_FLAG
enums['SERIAL_CONTROL_FLAG'] = {}
SERIAL_CONTROL_FLAG_REPLY = 1 # Set if this is a reply
enums['SERIAL_CONTROL_FLAG'][1] = EnumEntry('SERIAL_CONTROL_FLAG_REPLY', '''Set if this is a reply''')
SERIAL_CONTROL_FLAG_RESPOND = 2 # Set if the sender wants the receiver to send a response as another
                        # SERIAL_CONTROL message
enums['SERIAL_CONTROL_FLAG'][2] = EnumEntry('SERIAL_CONTROL_FLAG_RESPOND', '''Set if the sender wants the receiver to send a response as another SERIAL_CONTROL message''')
SERIAL_CONTROL_FLAG_EXCLUSIVE = 4 # Set if access to the serial port should be removed from whatever
                        # driver is currently using it, giving
                        # exclusive access to the SERIAL_CONTROL
                        # protocol. The port can be handed back by
                        # sending a request without this flag set
enums['SERIAL_CONTROL_FLAG'][4] = EnumEntry('SERIAL_CONTROL_FLAG_EXCLUSIVE', '''Set if access to the serial port should be removed from whatever driver is currently using it, giving exclusive access to the SERIAL_CONTROL protocol. The port can be handed back by sending a request without this flag set''')
SERIAL_CONTROL_FLAG_BLOCKING = 8 # Block on writes to the serial port
enums['SERIAL_CONTROL_FLAG'][8] = EnumEntry('SERIAL_CONTROL_FLAG_BLOCKING', '''Block on writes to the serial port''')
SERIAL_CONTROL_FLAG_MULTI = 16 # Send multiple replies until port is drained
enums['SERIAL_CONTROL_FLAG'][16] = EnumEntry('SERIAL_CONTROL_FLAG_MULTI', '''Send multiple replies until port is drained''')
SERIAL_CONTROL_FLAG_ENUM_END = 17 # 
enums['SERIAL_CONTROL_FLAG'][17] = EnumEntry('SERIAL_CONTROL_FLAG_ENUM_END', '''''')

# MAV_DISTANCE_SENSOR
enums['MAV_DISTANCE_SENSOR'] = {}
MAV_DISTANCE_SENSOR_LASER = 0 # Laser rangefinder, e.g. LightWare SF02/F or PulsedLight units
enums['MAV_DISTANCE_SENSOR'][0] = EnumEntry('MAV_DISTANCE_SENSOR_LASER', '''Laser rangefinder, e.g. LightWare SF02/F or PulsedLight units''')
MAV_DISTANCE_SENSOR_ULTRASOUND = 1 # Ultrasound rangefinder, e.g. MaxBotix units
enums['MAV_DISTANCE_SENSOR'][1] = EnumEntry('MAV_DISTANCE_SENSOR_ULTRASOUND', '''Ultrasound rangefinder, e.g. MaxBotix units''')
MAV_DISTANCE_SENSOR_INFRARED = 2 # Infrared rangefinder, e.g. Sharp units
enums['MAV_DISTANCE_SENSOR'][2] = EnumEntry('MAV_DISTANCE_SENSOR_INFRARED', '''Infrared rangefinder, e.g. Sharp units''')
MAV_DISTANCE_SENSOR_ENUM_END = 3 # 
enums['MAV_DISTANCE_SENSOR'][3] = EnumEntry('MAV_DISTANCE_SENSOR_ENUM_END', '''''')

# MAV_SENSOR_ORIENTATION
enums['MAV_SENSOR_ORIENTATION'] = {}
MAV_SENSOR_ROTATION_NONE = 0 # Roll: 0, Pitch: 0, Yaw: 0
enums['MAV_SENSOR_ORIENTATION'][0] = EnumEntry('MAV_SENSOR_ROTATION_NONE', '''Roll: 0, Pitch: 0, Yaw: 0''')
MAV_SENSOR_ROTATION_YAW_45 = 1 # Roll: 0, Pitch: 0, Yaw: 45
enums['MAV_SENSOR_ORIENTATION'][1] = EnumEntry('MAV_SENSOR_ROTATION_YAW_45', '''Roll: 0, Pitch: 0, Yaw: 45''')
MAV_SENSOR_ROTATION_YAW_90 = 2 # Roll: 0, Pitch: 0, Yaw: 90
enums['MAV_SENSOR_ORIENTATION'][2] = EnumEntry('MAV_SENSOR_ROTATION_YAW_90', '''Roll: 0, Pitch: 0, Yaw: 90''')
MAV_SENSOR_ROTATION_YAW_135 = 3 # Roll: 0, Pitch: 0, Yaw: 135
enums['MAV_SENSOR_ORIENTATION'][3] = EnumEntry('MAV_SENSOR_ROTATION_YAW_135', '''Roll: 0, Pitch: 0, Yaw: 135''')
MAV_SENSOR_ROTATION_YAW_180 = 4 # Roll: 0, Pitch: 0, Yaw: 180
enums['MAV_SENSOR_ORIENTATION'][4] = EnumEntry('MAV_SENSOR_ROTATION_YAW_180', '''Roll: 0, Pitch: 0, Yaw: 180''')
MAV_SENSOR_ROTATION_YAW_225 = 5 # Roll: 0, Pitch: 0, Yaw: 225
enums['MAV_SENSOR_ORIENTATION'][5] = EnumEntry('MAV_SENSOR_ROTATION_YAW_225', '''Roll: 0, Pitch: 0, Yaw: 225''')
MAV_SENSOR_ROTATION_YAW_270 = 6 # Roll: 0, Pitch: 0, Yaw: 270
enums['MAV_SENSOR_ORIENTATION'][6] = EnumEntry('MAV_SENSOR_ROTATION_YAW_270', '''Roll: 0, Pitch: 0, Yaw: 270''')
MAV_SENSOR_ROTATION_YAW_315 = 7 # Roll: 0, Pitch: 0, Yaw: 315
enums['MAV_SENSOR_ORIENTATION'][7] = EnumEntry('MAV_SENSOR_ROTATION_YAW_315', '''Roll: 0, Pitch: 0, Yaw: 315''')
MAV_SENSOR_ROTATION_ROLL_180 = 8 # Roll: 180, Pitch: 0, Yaw: 0
enums['MAV_SENSOR_ORIENTATION'][8] = EnumEntry('MAV_SENSOR_ROTATION_ROLL_180', '''Roll: 180, Pitch: 0, Yaw: 0''')
MAV_SENSOR_ROTATION_ROLL_180_YAW_45 = 9 # Roll: 180, Pitch: 0, Yaw: 45
enums['MAV_SENSOR_ORIENTATION'][9] = EnumEntry('MAV_SENSOR_ROTATION_ROLL_180_YAW_45', '''Roll: 180, Pitch: 0, Yaw: 45''')
MAV_SENSOR_ROTATION_ROLL_180_YAW_90 = 10 # Roll: 180, Pitch: 0, Yaw: 90
enums['MAV_SENSOR_ORIENTATION'][10] = EnumEntry('MAV_SENSOR_ROTATION_ROLL_180_YAW_90', '''Roll: 180, Pitch: 0, Yaw: 90''')
MAV_SENSOR_ROTATION_ROLL_180_YAW_135 = 11 # Roll: 180, Pitch: 0, Yaw: 135
enums['MAV_SENSOR_ORIENTATION'][11] = EnumEntry('MAV_SENSOR_ROTATION_ROLL_180_YAW_135', '''Roll: 180, Pitch: 0, Yaw: 135''')
MAV_SENSOR_ROTATION_PITCH_180 = 12 # Roll: 0, Pitch: 180, Yaw: 0
enums['MAV_SENSOR_ORIENTATION'][12] = EnumEntry('MAV_SENSOR_ROTATION_PITCH_180', '''Roll: 0, Pitch: 180, Yaw: 0''')
MAV_SENSOR_ROTATION_ROLL_180_YAW_225 = 13 # Roll: 180, Pitch: 0, Yaw: 225
enums['MAV_SENSOR_ORIENTATION'][13] = EnumEntry('MAV_SENSOR_ROTATION_ROLL_180_YAW_225', '''Roll: 180, Pitch: 0, Yaw: 225''')
MAV_SENSOR_ROTATION_ROLL_180_YAW_270 = 14 # Roll: 180, Pitch: 0, Yaw: 270
enums['MAV_SENSOR_ORIENTATION'][14] = EnumEntry('MAV_SENSOR_ROTATION_ROLL_180_YAW_270', '''Roll: 180, Pitch: 0, Yaw: 270''')
MAV_SENSOR_ROTATION_ROLL_180_YAW_315 = 15 # Roll: 180, Pitch: 0, Yaw: 315
enums['MAV_SENSOR_ORIENTATION'][15] = EnumEntry('MAV_SENSOR_ROTATION_ROLL_180_YAW_315', '''Roll: 180, Pitch: 0, Yaw: 315''')
MAV_SENSOR_ROTATION_ROLL_90 = 16 # Roll: 90, Pitch: 0, Yaw: 0
enums['MAV_SENSOR_ORIENTATION'][16] = EnumEntry('MAV_SENSOR_ROTATION_ROLL_90', '''Roll: 90, Pitch: 0, Yaw: 0''')
MAV_SENSOR_ROTATION_ROLL_90_YAW_45 = 17 # Roll: 90, Pitch: 0, Yaw: 45
enums['MAV_SENSOR_ORIENTATION'][17] = EnumEntry('MAV_SENSOR_ROTATION_ROLL_90_YAW_45', '''Roll: 90, Pitch: 0, Yaw: 45''')
MAV_SENSOR_ROTATION_ROLL_90_YAW_90 = 18 # Roll: 90, Pitch: 0, Yaw: 90
enums['MAV_SENSOR_ORIENTATION'][18] = EnumEntry('MAV_SENSOR_ROTATION_ROLL_90_YAW_90', '''Roll: 90, Pitch: 0, Yaw: 90''')
MAV_SENSOR_ROTATION_ROLL_90_YAW_135 = 19 # Roll: 90, Pitch: 0, Yaw: 135
enums['MAV_SENSOR_ORIENTATION'][19] = EnumEntry('MAV_SENSOR_ROTATION_ROLL_90_YAW_135', '''Roll: 90, Pitch: 0, Yaw: 135''')
MAV_SENSOR_ROTATION_ROLL_270 = 20 # Roll: 270, Pitch: 0, Yaw: 0
enums['MAV_SENSOR_ORIENTATION'][20] = EnumEntry('MAV_SENSOR_ROTATION_ROLL_270', '''Roll: 270, Pitch: 0, Yaw: 0''')
MAV_SENSOR_ROTATION_ROLL_270_YAW_45 = 21 # Roll: 270, Pitch: 0, Yaw: 45
enums['MAV_SENSOR_ORIENTATION'][21] = EnumEntry('MAV_SENSOR_ROTATION_ROLL_270_YAW_45', '''Roll: 270, Pitch: 0, Yaw: 45''')
MAV_SENSOR_ROTATION_ROLL_270_YAW_90 = 22 # Roll: 270, Pitch: 0, Yaw: 90
enums['MAV_SENSOR_ORIENTATION'][22] = EnumEntry('MAV_SENSOR_ROTATION_ROLL_270_YAW_90', '''Roll: 270, Pitch: 0, Yaw: 90''')
MAV_SENSOR_ROTATION_ROLL_270_YAW_135 = 23 # Roll: 270, Pitch: 0, Yaw: 135
enums['MAV_SENSOR_ORIENTATION'][23] = EnumEntry('MAV_SENSOR_ROTATION_ROLL_270_YAW_135', '''Roll: 270, Pitch: 0, Yaw: 135''')
MAV_SENSOR_ROTATION_PITCH_90 = 24 # Roll: 0, Pitch: 90, Yaw: 0
enums['MAV_SENSOR_ORIENTATION'][24] = EnumEntry('MAV_SENSOR_ROTATION_PITCH_90', '''Roll: 0, Pitch: 90, Yaw: 0''')
MAV_SENSOR_ROTATION_PITCH_270 = 25 # Roll: 0, Pitch: 270, Yaw: 0
enums['MAV_SENSOR_ORIENTATION'][25] = EnumEntry('MAV_SENSOR_ROTATION_PITCH_270', '''Roll: 0, Pitch: 270, Yaw: 0''')
MAV_SENSOR_ROTATION_PITCH_180_YAW_90 = 26 # Roll: 0, Pitch: 180, Yaw: 90
enums['MAV_SENSOR_ORIENTATION'][26] = EnumEntry('MAV_SENSOR_ROTATION_PITCH_180_YAW_90', '''Roll: 0, Pitch: 180, Yaw: 90''')
MAV_SENSOR_ROTATION_PITCH_180_YAW_270 = 27 # Roll: 0, Pitch: 180, Yaw: 270
enums['MAV_SENSOR_ORIENTATION'][27] = EnumEntry('MAV_SENSOR_ROTATION_PITCH_180_YAW_270', '''Roll: 0, Pitch: 180, Yaw: 270''')
MAV_SENSOR_ROTATION_ROLL_90_PITCH_90 = 28 # Roll: 90, Pitch: 90, Yaw: 0
enums['MAV_SENSOR_ORIENTATION'][28] = EnumEntry('MAV_SENSOR_ROTATION_ROLL_90_PITCH_90', '''Roll: 90, Pitch: 90, Yaw: 0''')
MAV_SENSOR_ROTATION_ROLL_180_PITCH_90 = 29 # Roll: 180, Pitch: 90, Yaw: 0
enums['MAV_SENSOR_ORIENTATION'][29] = EnumEntry('MAV_SENSOR_ROTATION_ROLL_180_PITCH_90', '''Roll: 180, Pitch: 90, Yaw: 0''')
MAV_SENSOR_ROTATION_ROLL_270_PITCH_90 = 30 # Roll: 270, Pitch: 90, Yaw: 0
enums['MAV_SENSOR_ORIENTATION'][30] = EnumEntry('MAV_SENSOR_ROTATION_ROLL_270_PITCH_90', '''Roll: 270, Pitch: 90, Yaw: 0''')
MAV_SENSOR_ROTATION_ROLL_90_PITCH_180 = 31 # Roll: 90, Pitch: 180, Yaw: 0
enums['MAV_SENSOR_ORIENTATION'][31] = EnumEntry('MAV_SENSOR_ROTATION_ROLL_90_PITCH_180', '''Roll: 90, Pitch: 180, Yaw: 0''')
MAV_SENSOR_ROTATION_ROLL_270_PITCH_180 = 32 # Roll: 270, Pitch: 180, Yaw: 0
enums['MAV_SENSOR_ORIENTATION'][32] = EnumEntry('MAV_SENSOR_ROTATION_ROLL_270_PITCH_180', '''Roll: 270, Pitch: 180, Yaw: 0''')
MAV_SENSOR_ROTATION_ROLL_90_PITCH_270 = 33 # Roll: 90, Pitch: 270, Yaw: 0
enums['MAV_SENSOR_ORIENTATION'][33] = EnumEntry('MAV_SENSOR_ROTATION_ROLL_90_PITCH_270', '''Roll: 90, Pitch: 270, Yaw: 0''')
MAV_SENSOR_ROTATION_ROLL_180_PITCH_270 = 34 # Roll: 180, Pitch: 270, Yaw: 0
enums['MAV_SENSOR_ORIENTATION'][34] = EnumEntry('MAV_SENSOR_ROTATION_ROLL_180_PITCH_270', '''Roll: 180, Pitch: 270, Yaw: 0''')
MAV_SENSOR_ROTATION_ROLL_270_PITCH_270 = 35 # Roll: 270, Pitch: 270, Yaw: 0
enums['MAV_SENSOR_ORIENTATION'][35] = EnumEntry('MAV_SENSOR_ROTATION_ROLL_270_PITCH_270', '''Roll: 270, Pitch: 270, Yaw: 0''')
MAV_SENSOR_ROTATION_ROLL_90_PITCH_180_YAW_90 = 36 # Roll: 90, Pitch: 180, Yaw: 90
enums['MAV_SENSOR_ORIENTATION'][36] = EnumEntry('MAV_SENSOR_ROTATION_ROLL_90_PITCH_180_YAW_90', '''Roll: 90, Pitch: 180, Yaw: 90''')
MAV_SENSOR_ROTATION_ROLL_90_YAW_270 = 37 # Roll: 90, Pitch: 0, Yaw: 270
enums['MAV_SENSOR_ORIENTATION'][37] = EnumEntry('MAV_SENSOR_ROTATION_ROLL_90_YAW_270', '''Roll: 90, Pitch: 0, Yaw: 270''')
MAV_SENSOR_ROTATION_ROLL_315_PITCH_315_YAW_315 = 38 # Roll: 315, Pitch: 315, Yaw: 315
enums['MAV_SENSOR_ORIENTATION'][38] = EnumEntry('MAV_SENSOR_ROTATION_ROLL_315_PITCH_315_YAW_315', '''Roll: 315, Pitch: 315, Yaw: 315''')
MAV_SENSOR_ORIENTATION_ENUM_END = 39 # 
enums['MAV_SENSOR_ORIENTATION'][39] = EnumEntry('MAV_SENSOR_ORIENTATION_ENUM_END', '''''')

# MAV_PROTOCOL_CAPABILITY
enums['MAV_PROTOCOL_CAPABILITY'] = {}
MAV_PROTOCOL_CAPABILITY_MISSION_FLOAT = 1 # Autopilot supports MISSION float message type.
enums['MAV_PROTOCOL_CAPABILITY'][1] = EnumEntry('MAV_PROTOCOL_CAPABILITY_MISSION_FLOAT', '''Autopilot supports MISSION float message type.''')
MAV_PROTOCOL_CAPABILITY_PARAM_FLOAT = 2 # Autopilot supports the new param float message type.
enums['MAV_PROTOCOL_CAPABILITY'][2] = EnumEntry('MAV_PROTOCOL_CAPABILITY_PARAM_FLOAT', '''Autopilot supports the new param float message type.''')
MAV_PROTOCOL_CAPABILITY_MISSION_INT = 4 # Autopilot supports MISSION_INT scaled integer message type.
enums['MAV_PROTOCOL_CAPABILITY'][4] = EnumEntry('MAV_PROTOCOL_CAPABILITY_MISSION_INT', '''Autopilot supports MISSION_INT scaled integer message type.''')
MAV_PROTOCOL_CAPABILITY_COMMAND_INT = 8 # Autopilot supports COMMAND_INT scaled integer message type.
enums['MAV_PROTOCOL_CAPABILITY'][8] = EnumEntry('MAV_PROTOCOL_CAPABILITY_COMMAND_INT', '''Autopilot supports COMMAND_INT scaled integer message type.''')
MAV_PROTOCOL_CAPABILITY_PARAM_UNION = 16 # Autopilot supports the new param union message type.
enums['MAV_PROTOCOL_CAPABILITY'][16] = EnumEntry('MAV_PROTOCOL_CAPABILITY_PARAM_UNION', '''Autopilot supports the new param union message type.''')
MAV_PROTOCOL_CAPABILITY_FTP = 32 # Autopilot supports the new param union message type.
enums['MAV_PROTOCOL_CAPABILITY'][32] = EnumEntry('MAV_PROTOCOL_CAPABILITY_FTP', '''Autopilot supports the new param union message type.''')
MAV_PROTOCOL_CAPABILITY_SET_ATTITUDE_TARGET = 64 # Autopilot supports commanding attitude offboard.
enums['MAV_PROTOCOL_CAPABILITY'][64] = EnumEntry('MAV_PROTOCOL_CAPABILITY_SET_ATTITUDE_TARGET', '''Autopilot supports commanding attitude offboard.''')
MAV_PROTOCOL_CAPABILITY_SET_POSITION_TARGET_LOCAL_NED = 128 # Autopilot supports commanding position and velocity targets in local
                        # NED frame.
enums['MAV_PROTOCOL_CAPABILITY'][128] = EnumEntry('MAV_PROTOCOL_CAPABILITY_SET_POSITION_TARGET_LOCAL_NED', '''Autopilot supports commanding position and velocity targets in local NED frame.''')
MAV_PROTOCOL_CAPABILITY_SET_POSITION_TARGET_GLOBAL_INT = 256 # Autopilot supports commanding position and velocity targets in global
                        # scaled integers.
enums['MAV_PROTOCOL_CAPABILITY'][256] = EnumEntry('MAV_PROTOCOL_CAPABILITY_SET_POSITION_TARGET_GLOBAL_INT', '''Autopilot supports commanding position and velocity targets in global scaled integers.''')
MAV_PROTOCOL_CAPABILITY_TERRAIN = 512 # Autopilot supports terrain protocol / data handling.
enums['MAV_PROTOCOL_CAPABILITY'][512] = EnumEntry('MAV_PROTOCOL_CAPABILITY_TERRAIN', '''Autopilot supports terrain protocol / data handling.''')
MAV_PROTOCOL_CAPABILITY_SET_ACTUATOR_TARGET = 1024 # Autopilot supports direct actuator control.
enums['MAV_PROTOCOL_CAPABILITY'][1024] = EnumEntry('MAV_PROTOCOL_CAPABILITY_SET_ACTUATOR_TARGET', '''Autopilot supports direct actuator control.''')
MAV_PROTOCOL_CAPABILITY_ENUM_END = 1025 # 
enums['MAV_PROTOCOL_CAPABILITY'][1025] = EnumEntry('MAV_PROTOCOL_CAPABILITY_ENUM_END', '''''')

# MAV_ESTIMATOR_TYPE
enums['MAV_ESTIMATOR_TYPE'] = {}
MAV_ESTIMATOR_TYPE_NAIVE = 1 # This is a naive estimator without any real covariance feedback.
enums['MAV_ESTIMATOR_TYPE'][1] = EnumEntry('MAV_ESTIMATOR_TYPE_NAIVE', '''This is a naive estimator without any real covariance feedback.''')
MAV_ESTIMATOR_TYPE_VISION = 2 # Computer vision based estimate. Might be up to scale.
enums['MAV_ESTIMATOR_TYPE'][2] = EnumEntry('MAV_ESTIMATOR_TYPE_VISION', '''Computer vision based estimate. Might be up to scale.''')
MAV_ESTIMATOR_TYPE_VIO = 3 # Visual-inertial estimate.
enums['MAV_ESTIMATOR_TYPE'][3] = EnumEntry('MAV_ESTIMATOR_TYPE_VIO', '''Visual-inertial estimate.''')
MAV_ESTIMATOR_TYPE_GPS = 4 # Plain GPS estimate.
enums['MAV_ESTIMATOR_TYPE'][4] = EnumEntry('MAV_ESTIMATOR_TYPE_GPS', '''Plain GPS estimate.''')
MAV_ESTIMATOR_TYPE_GPS_INS = 5 # Estimator integrating GPS and inertial sensing.
enums['MAV_ESTIMATOR_TYPE'][5] = EnumEntry('MAV_ESTIMATOR_TYPE_GPS_INS', '''Estimator integrating GPS and inertial sensing.''')
MAV_ESTIMATOR_TYPE_ENUM_END = 6 # 
enums['MAV_ESTIMATOR_TYPE'][6] = EnumEntry('MAV_ESTIMATOR_TYPE_ENUM_END', '''''')

# MAV_BATTERY_TYPE
enums['MAV_BATTERY_TYPE'] = {}
MAV_BATTERY_TYPE_UNKNOWN = 0 # Not specified.
enums['MAV_BATTERY_TYPE'][0] = EnumEntry('MAV_BATTERY_TYPE_UNKNOWN', '''Not specified.''')
MAV_BATTERY_TYPE_LIPO = 1 # Lithium polymere battery
enums['MAV_BATTERY_TYPE'][1] = EnumEntry('MAV_BATTERY_TYPE_LIPO', '''Lithium polymere battery''')
MAV_BATTERY_TYPE_LIFE = 2 # Lithium ferrite battery
enums['MAV_BATTERY_TYPE'][2] = EnumEntry('MAV_BATTERY_TYPE_LIFE', '''Lithium ferrite battery''')
MAV_BATTERY_TYPE_LION = 3 # Lithium-ION battery
enums['MAV_BATTERY_TYPE'][3] = EnumEntry('MAV_BATTERY_TYPE_LION', '''Lithium-ION battery''')
MAV_BATTERY_TYPE_NIMH = 4 # Nickel metal hydride battery
enums['MAV_BATTERY_TYPE'][4] = EnumEntry('MAV_BATTERY_TYPE_NIMH', '''Nickel metal hydride battery''')
MAV_BATTERY_TYPE_ENUM_END = 5 # 
enums['MAV_BATTERY_TYPE'][5] = EnumEntry('MAV_BATTERY_TYPE_ENUM_END', '''''')

# MAV_BATTERY_FUNCTION
enums['MAV_BATTERY_FUNCTION'] = {}
MAV_BATTERY_FUNCTION_UNKNOWN = 0 # Lithium polymere battery
enums['MAV_BATTERY_FUNCTION'][0] = EnumEntry('MAV_BATTERY_FUNCTION_UNKNOWN', '''Lithium polymere battery''')
MAV_BATTERY_FUNCTION_ALL = 1 # Battery supports all flight systems
enums['MAV_BATTERY_FUNCTION'][1] = EnumEntry('MAV_BATTERY_FUNCTION_ALL', '''Battery supports all flight systems''')
MAV_BATTERY_FUNCTION_PROPULSION = 2 # Battery for the propulsion system
enums['MAV_BATTERY_FUNCTION'][2] = EnumEntry('MAV_BATTERY_FUNCTION_PROPULSION', '''Battery for the propulsion system''')
MAV_BATTERY_FUNCTION_AVIONICS = 3 # Avionics battery
enums['MAV_BATTERY_FUNCTION'][3] = EnumEntry('MAV_BATTERY_FUNCTION_AVIONICS', '''Avionics battery''')
MAV_BATTERY_TYPE_PAYLOAD = 4 # Payload battery
enums['MAV_BATTERY_FUNCTION'][4] = EnumEntry('MAV_BATTERY_TYPE_PAYLOAD', '''Payload battery''')
MAV_BATTERY_FUNCTION_ENUM_END = 5 # 
enums['MAV_BATTERY_FUNCTION'][5] = EnumEntry('MAV_BATTERY_FUNCTION_ENUM_END', '''''')

# message IDs
MAVLINK_MSG_ID_BAD_DATA = -1
MAVLINK_MSG_ID_HEARTBEAT = 0
MAVLINK_MSG_ID_SYS_STATUS = 1
MAVLINK_MSG_ID_SYSTEM_TIME = 2
MAVLINK_MSG_ID_PING = 4
MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL = 5
MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL_ACK = 6
MAVLINK_MSG_ID_AUTH_KEY = 7
MAVLINK_MSG_ID_SET_MODE = 11
MAVLINK_MSG_ID_PARAM_REQUEST_READ = 20
MAVLINK_MSG_ID_PARAM_REQUEST_LIST = 21
MAVLINK_MSG_ID_PARAM_VALUE = 22
MAVLINK_MSG_ID_PARAM_SET = 23
MAVLINK_MSG_ID_GPS_RAW_INT = 24
MAVLINK_MSG_ID_GPS_STATUS = 25
MAVLINK_MSG_ID_SCALED_IMU = 26
MAVLINK_MSG_ID_RAW_IMU = 27
MAVLINK_MSG_ID_RAW_PRESSURE = 28
MAVLINK_MSG_ID_SCALED_PRESSURE = 29
MAVLINK_MSG_ID_ATTITUDE = 30
MAVLINK_MSG_ID_ATTITUDE_QUATERNION = 31
MAVLINK_MSG_ID_LOCAL_POSITION_NED = 32
MAVLINK_MSG_ID_GLOBAL_POSITION_INT = 33
MAVLINK_MSG_ID_RC_CHANNELS_SCALED = 34
MAVLINK_MSG_ID_RC_CHANNELS_RAW = 35
MAVLINK_MSG_ID_SERVO_OUTPUT_RAW = 36
MAVLINK_MSG_ID_MISSION_REQUEST_PARTIAL_LIST = 37
MAVLINK_MSG_ID_MISSION_WRITE_PARTIAL_LIST = 38
MAVLINK_MSG_ID_MISSION_ITEM = 39
MAVLINK_MSG_ID_MISSION_REQUEST = 40
MAVLINK_MSG_ID_MISSION_SET_CURRENT = 41
MAVLINK_MSG_ID_MISSION_CURRENT = 42
MAVLINK_MSG_ID_MISSION_REQUEST_LIST = 43
MAVLINK_MSG_ID_MISSION_COUNT = 44
MAVLINK_MSG_ID_MISSION_CLEAR_ALL = 45
MAVLINK_MSG_ID_MISSION_ITEM_REACHED = 46
MAVLINK_MSG_ID_MISSION_ACK = 47
MAVLINK_MSG_ID_SET_GPS_GLOBAL_ORIGIN = 48
MAVLINK_MSG_ID_GPS_GLOBAL_ORIGIN = 49
MAVLINK_MSG_ID_PARAM_MAP_RC = 50
MAVLINK_MSG_ID_SAFETY_SET_ALLOWED_AREA = 54
MAVLINK_MSG_ID_SAFETY_ALLOWED_AREA = 55
MAVLINK_MSG_ID_ATTITUDE_QUATERNION_COV = 61
MAVLINK_MSG_ID_NAV_CONTROLLER_OUTPUT = 62
MAVLINK_MSG_ID_GLOBAL_POSITION_INT_COV = 63
MAVLINK_MSG_ID_LOCAL_POSITION_NED_COV = 64
MAVLINK_MSG_ID_RC_CHANNELS = 65
MAVLINK_MSG_ID_REQUEST_DATA_STREAM = 66
MAVLINK_MSG_ID_DATA_STREAM = 67
MAVLINK_MSG_ID_MANUAL_CONTROL = 69
MAVLINK_MSG_ID_RC_CHANNELS_OVERRIDE = 70
MAVLINK_MSG_ID_MISSION_ITEM_INT = 73
MAVLINK_MSG_ID_VFR_HUD = 74
MAVLINK_MSG_ID_COMMAND_INT = 75
MAVLINK_MSG_ID_COMMAND_LONG = 76
MAVLINK_MSG_ID_COMMAND_ACK = 77
MAVLINK_MSG_ID_MANUAL_SETPOINT = 81
MAVLINK_MSG_ID_SET_ATTITUDE_TARGET = 82
MAVLINK_MSG_ID_ATTITUDE_TARGET = 83
MAVLINK_MSG_ID_SET_POSITION_TARGET_LOCAL_NED = 84
MAVLINK_MSG_ID_POSITION_TARGET_LOCAL_NED = 85
MAVLINK_MSG_ID_SET_POSITION_TARGET_GLOBAL_INT = 86
MAVLINK_MSG_ID_POSITION_TARGET_GLOBAL_INT = 87
MAVLINK_MSG_ID_LOCAL_POSITION_NED_SYSTEM_GLOBAL_OFFSET = 89
MAVLINK_MSG_ID_HIL_STATE = 90
MAVLINK_MSG_ID_HIL_CONTROLS = 91
MAVLINK_MSG_ID_HIL_RC_INPUTS_RAW = 92
MAVLINK_MSG_ID_OPTICAL_FLOW = 100
MAVLINK_MSG_ID_GLOBAL_VISION_POSITION_ESTIMATE = 101
MAVLINK_MSG_ID_VISION_POSITION_ESTIMATE = 102
MAVLINK_MSG_ID_VISION_SPEED_ESTIMATE = 103
MAVLINK_MSG_ID_VICON_POSITION_ESTIMATE = 104
MAVLINK_MSG_ID_HIGHRES_IMU = 105
MAVLINK_MSG_ID_OPTICAL_FLOW_RAD = 106
MAVLINK_MSG_ID_HIL_SENSOR = 107
MAVLINK_MSG_ID_SIM_STATE = 108
MAVLINK_MSG_ID_RADIO_STATUS = 109
MAVLINK_MSG_ID_FILE_TRANSFER_PROTOCOL = 110
MAVLINK_MSG_ID_TIMESYNC = 111
MAVLINK_MSG_ID_CAMERA_TRIGGER = 112
MAVLINK_MSG_ID_HIL_GPS = 113
MAVLINK_MSG_ID_HIL_OPTICAL_FLOW = 114
MAVLINK_MSG_ID_HIL_STATE_QUATERNION = 115
MAVLINK_MSG_ID_SCALED_IMU2 = 116
MAVLINK_MSG_ID_LOG_REQUEST_LIST = 117
MAVLINK_MSG_ID_LOG_ENTRY = 118
MAVLINK_MSG_ID_LOG_REQUEST_DATA = 119
MAVLINK_MSG_ID_LOG_DATA = 120
MAVLINK_MSG_ID_LOG_ERASE = 121
MAVLINK_MSG_ID_LOG_REQUEST_END = 122
MAVLINK_MSG_ID_GPS_INJECT_DATA = 123
MAVLINK_MSG_ID_GPS2_RAW = 124
MAVLINK_MSG_ID_POWER_STATUS = 125
MAVLINK_MSG_ID_SERIAL_CONTROL = 126
MAVLINK_MSG_ID_GPS_RTK = 127
MAVLINK_MSG_ID_GPS2_RTK = 128
MAVLINK_MSG_ID_SCALED_IMU3 = 129
MAVLINK_MSG_ID_DATA_TRANSMISSION_HANDSHAKE = 130
MAVLINK_MSG_ID_ENCAPSULATED_DATA = 131
MAVLINK_MSG_ID_DISTANCE_SENSOR = 132
MAVLINK_MSG_ID_TERRAIN_REQUEST = 133
MAVLINK_MSG_ID_TERRAIN_DATA = 134
MAVLINK_MSG_ID_TERRAIN_CHECK = 135
MAVLINK_MSG_ID_TERRAIN_REPORT = 136
MAVLINK_MSG_ID_SCALED_PRESSURE2 = 137
MAVLINK_MSG_ID_ATT_POS_MOCAP = 138
MAVLINK_MSG_ID_SET_ACTUATOR_CONTROL_TARGET = 139
MAVLINK_MSG_ID_ACTUATOR_CONTROL_TARGET = 140
MAVLINK_MSG_ID_BATTERY_STATUS = 147
MAVLINK_MSG_ID_AUTOPILOT_VERSION = 148
MAVLINK_MSG_ID_LANDING_TARGET = 149
MAVLINK_MSG_ID_VIBRATION = 241
MAVLINK_MSG_ID_V2_EXTENSION = 248
MAVLINK_MSG_ID_MEMORY_VECT = 249
MAVLINK_MSG_ID_DEBUG_VECT = 250
MAVLINK_MSG_ID_NAMED_VALUE_FLOAT = 251
MAVLINK_MSG_ID_NAMED_VALUE_INT = 252
MAVLINK_MSG_ID_STATUSTEXT = 253
MAVLINK_MSG_ID_DEBUG = 254

class MAVLink_heartbeat_message(MAVLink_message):
        '''
        The heartbeat message shows that a system is present and
        responding. The type of the MAV and Autopilot hardware allow
        the receiving system to treat further messages from this
        system appropriate (e.g. by laying out the user interface
        based on the autopilot).
        '''
        id = MAVLINK_MSG_ID_HEARTBEAT
        name = 'HEARTBEAT'
        fieldnames = ['type', 'autopilot', 'base_mode', 'custom_mode', 'system_status', 'mavlink_version']
        ordered_fieldnames = [ 'custom_mode', 'type', 'autopilot', 'base_mode', 'system_status', 'mavlink_version' ]
        format = '<IBBBBB'
        native_format = bytearray('<IBBBBB', 'ascii')
        orders = [1, 2, 3, 0, 4, 5]
        lengths = [1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0]
        crc_extra = 50

        def __init__(self, type, autopilot, base_mode, custom_mode, system_status, mavlink_version):
                MAVLink_message.__init__(self, MAVLink_heartbeat_message.id, MAVLink_heartbeat_message.name)
                self._fieldnames = MAVLink_heartbeat_message.fieldnames
                self.type = type
                self.autopilot = autopilot
                self.base_mode = base_mode
                self.custom_mode = custom_mode
                self.system_status = system_status
                self.mavlink_version = mavlink_version

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 50, struct.pack('<IBBBBB', self.custom_mode, self.type, self.autopilot, self.base_mode, self.system_status, self.mavlink_version))

class MAVLink_sys_status_message(MAVLink_message):
        '''
        The general system state. If the system is following the
        MAVLink standard, the system state is mainly defined by three
        orthogonal states/modes: The system mode, which is either
        LOCKED (motors shut down and locked), MANUAL (system under RC
        control), GUIDED (system with autonomous position control,
        position setpoint controlled manually) or AUTO (system guided
        by path/waypoint planner). The NAV_MODE defined the current
        flight state: LIFTOFF (often an open-loop maneuver), LANDING,
        WAYPOINTS or VECTOR. This represents the internal navigation
        state machine. The system status shows wether the system is
        currently active or not and if an emergency occured. During
        the CRITICAL and EMERGENCY states the MAV is still considered
        to be active, but should start emergency procedures
        autonomously. After a failure occured it should first move
        from active to critical to allow manual intervention and then
        move to emergency after a certain timeout.
        '''
        id = MAVLINK_MSG_ID_SYS_STATUS
        name = 'SYS_STATUS'
        fieldnames = ['onboard_control_sensors_present', 'onboard_control_sensors_enabled', 'onboard_control_sensors_health', 'load', 'voltage_battery', 'current_battery', 'battery_remaining', 'drop_rate_comm', 'errors_comm', 'errors_count1', 'errors_count2', 'errors_count3', 'errors_count4']
        ordered_fieldnames = [ 'onboard_control_sensors_present', 'onboard_control_sensors_enabled', 'onboard_control_sensors_health', 'load', 'voltage_battery', 'current_battery', 'drop_rate_comm', 'errors_comm', 'errors_count1', 'errors_count2', 'errors_count3', 'errors_count4', 'battery_remaining' ]
        format = '<IIIHHhHHHHHHb'
        native_format = bytearray('<IIIHHhHHHHHHb', 'ascii')
        orders = [0, 1, 2, 3, 4, 5, 12, 6, 7, 8, 9, 10, 11]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 124

        def __init__(self, onboard_control_sensors_present, onboard_control_sensors_enabled, onboard_control_sensors_health, load, voltage_battery, current_battery, battery_remaining, drop_rate_comm, errors_comm, errors_count1, errors_count2, errors_count3, errors_count4):
                MAVLink_message.__init__(self, MAVLink_sys_status_message.id, MAVLink_sys_status_message.name)
                self._fieldnames = MAVLink_sys_status_message.fieldnames
                self.onboard_control_sensors_present = onboard_control_sensors_present
                self.onboard_control_sensors_enabled = onboard_control_sensors_enabled
                self.onboard_control_sensors_health = onboard_control_sensors_health
                self.load = load
                self.voltage_battery = voltage_battery
                self.current_battery = current_battery
                self.battery_remaining = battery_remaining
                self.drop_rate_comm = drop_rate_comm
                self.errors_comm = errors_comm
                self.errors_count1 = errors_count1
                self.errors_count2 = errors_count2
                self.errors_count3 = errors_count3
                self.errors_count4 = errors_count4

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 124, struct.pack('<IIIHHhHHHHHHb', self.onboard_control_sensors_present, self.onboard_control_sensors_enabled, self.onboard_control_sensors_health, self.load, self.voltage_battery, self.current_battery, self.drop_rate_comm, self.errors_comm, self.errors_count1, self.errors_count2, self.errors_count3, self.errors_count4, self.battery_remaining))

class MAVLink_system_time_message(MAVLink_message):
        '''
        The system time is the time of the master clock, typically the
        computer clock of the main onboard computer.
        '''
        id = MAVLINK_MSG_ID_SYSTEM_TIME
        name = 'SYSTEM_TIME'
        fieldnames = ['time_unix_usec', 'time_boot_ms']
        ordered_fieldnames = [ 'time_unix_usec', 'time_boot_ms' ]
        format = '<QI'
        native_format = bytearray('<QI', 'ascii')
        orders = [0, 1]
        lengths = [1, 1]
        array_lengths = [0, 0]
        crc_extra = 137

        def __init__(self, time_unix_usec, time_boot_ms):
                MAVLink_message.__init__(self, MAVLink_system_time_message.id, MAVLink_system_time_message.name)
                self._fieldnames = MAVLink_system_time_message.fieldnames
                self.time_unix_usec = time_unix_usec
                self.time_boot_ms = time_boot_ms

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 137, struct.pack('<QI', self.time_unix_usec, self.time_boot_ms))

class MAVLink_ping_message(MAVLink_message):
        '''
        A ping message either requesting or responding to a ping. This
        allows to measure the system latencies, including serial port,
        radio modem and UDP connections.
        '''
        id = MAVLINK_MSG_ID_PING
        name = 'PING'
        fieldnames = ['time_usec', 'seq', 'target_system', 'target_component']
        ordered_fieldnames = [ 'time_usec', 'seq', 'target_system', 'target_component' ]
        format = '<QIBB'
        native_format = bytearray('<QIBB', 'ascii')
        orders = [0, 1, 2, 3]
        lengths = [1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0]
        crc_extra = 237

        def __init__(self, time_usec, seq, target_system, target_component):
                MAVLink_message.__init__(self, MAVLink_ping_message.id, MAVLink_ping_message.name)
                self._fieldnames = MAVLink_ping_message.fieldnames
                self.time_usec = time_usec
                self.seq = seq
                self.target_system = target_system
                self.target_component = target_component

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 237, struct.pack('<QIBB', self.time_usec, self.seq, self.target_system, self.target_component))

class MAVLink_change_operator_control_message(MAVLink_message):
        '''
        Request to control this MAV
        '''
        id = MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL
        name = 'CHANGE_OPERATOR_CONTROL'
        fieldnames = ['target_system', 'control_request', 'version', 'passkey']
        ordered_fieldnames = [ 'target_system', 'control_request', 'version', 'passkey' ]
        format = '<BBB25s'
        native_format = bytearray('<BBBc', 'ascii')
        orders = [0, 1, 2, 3]
        lengths = [1, 1, 1, 1]
        array_lengths = [0, 0, 0, 25]
        crc_extra = 217

        def __init__(self, target_system, control_request, version, passkey):
                MAVLink_message.__init__(self, MAVLink_change_operator_control_message.id, MAVLink_change_operator_control_message.name)
                self._fieldnames = MAVLink_change_operator_control_message.fieldnames
                self.target_system = target_system
                self.control_request = control_request
                self.version = version
                self.passkey = passkey

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 217, struct.pack('<BBB25s', self.target_system, self.control_request, self.version, self.passkey))

class MAVLink_change_operator_control_ack_message(MAVLink_message):
        '''
        Accept / deny control of this MAV
        '''
        id = MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL_ACK
        name = 'CHANGE_OPERATOR_CONTROL_ACK'
        fieldnames = ['gcs_system_id', 'control_request', 'ack']
        ordered_fieldnames = [ 'gcs_system_id', 'control_request', 'ack' ]
        format = '<BBB'
        native_format = bytearray('<BBB', 'ascii')
        orders = [0, 1, 2]
        lengths = [1, 1, 1]
        array_lengths = [0, 0, 0]
        crc_extra = 104

        def __init__(self, gcs_system_id, control_request, ack):
                MAVLink_message.__init__(self, MAVLink_change_operator_control_ack_message.id, MAVLink_change_operator_control_ack_message.name)
                self._fieldnames = MAVLink_change_operator_control_ack_message.fieldnames
                self.gcs_system_id = gcs_system_id
                self.control_request = control_request
                self.ack = ack

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 104, struct.pack('<BBB', self.gcs_system_id, self.control_request, self.ack))

class MAVLink_auth_key_message(MAVLink_message):
        '''
        Emit an encrypted signature / key identifying this system.
        PLEASE NOTE: This protocol has been kept simple, so
        transmitting the key requires an encrypted channel for true
        safety.
        '''
        id = MAVLINK_MSG_ID_AUTH_KEY
        name = 'AUTH_KEY'
        fieldnames = ['key']
        ordered_fieldnames = [ 'key' ]
        format = '<32s'
        native_format = bytearray('<c', 'ascii')
        orders = [0]
        lengths = [1]
        array_lengths = [32]
        crc_extra = 119

        def __init__(self, key):
                MAVLink_message.__init__(self, MAVLink_auth_key_message.id, MAVLink_auth_key_message.name)
                self._fieldnames = MAVLink_auth_key_message.fieldnames
                self.key = key

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 119, struct.pack('<32s', self.key))

class MAVLink_set_mode_message(MAVLink_message):
        '''
        Set the system mode, as defined by enum MAV_MODE. There is no
        target component id as the mode is by definition for the
        overall aircraft, not only for one component.
        '''
        id = MAVLINK_MSG_ID_SET_MODE
        name = 'SET_MODE'
        fieldnames = ['target_system', 'base_mode', 'custom_mode']
        ordered_fieldnames = [ 'custom_mode', 'target_system', 'base_mode' ]
        format = '<IBB'
        native_format = bytearray('<IBB', 'ascii')
        orders = [1, 2, 0]
        lengths = [1, 1, 1]
        array_lengths = [0, 0, 0]
        crc_extra = 89

        def __init__(self, target_system, base_mode, custom_mode):
                MAVLink_message.__init__(self, MAVLink_set_mode_message.id, MAVLink_set_mode_message.name)
                self._fieldnames = MAVLink_set_mode_message.fieldnames
                self.target_system = target_system
                self.base_mode = base_mode
                self.custom_mode = custom_mode

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 89, struct.pack('<IBB', self.custom_mode, self.target_system, self.base_mode))

class MAVLink_param_request_read_message(MAVLink_message):
        '''
        Request to read the onboard parameter with the param_id string
        id. Onboard parameters are stored as key[const char*] ->
        value[float]. This allows to send a parameter to any other
        component (such as the GCS) without the need of previous
        knowledge of possible parameter names. Thus the same GCS can
        store different parameters for different autopilots. See also
        http://qgroundcontrol.org/parameter_interface for a full
        documentation of QGroundControl and IMU code.
        '''
        id = MAVLINK_MSG_ID_PARAM_REQUEST_READ
        name = 'PARAM_REQUEST_READ'
        fieldnames = ['target_system', 'target_component', 'param_id', 'param_index']
        ordered_fieldnames = [ 'param_index', 'target_system', 'target_component', 'param_id' ]
        format = '<hBB16s'
        native_format = bytearray('<hBBc', 'ascii')
        orders = [1, 2, 3, 0]
        lengths = [1, 1, 1, 1]
        array_lengths = [0, 0, 0, 16]
        crc_extra = 214

        def __init__(self, target_system, target_component, param_id, param_index):
                MAVLink_message.__init__(self, MAVLink_param_request_read_message.id, MAVLink_param_request_read_message.name)
                self._fieldnames = MAVLink_param_request_read_message.fieldnames
                self.target_system = target_system
                self.target_component = target_component
                self.param_id = param_id
                self.param_index = param_index

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 214, struct.pack('<hBB16s', self.param_index, self.target_system, self.target_component, self.param_id))

class MAVLink_param_request_list_message(MAVLink_message):
        '''
        Request all parameters of this component. After his request,
        all parameters are emitted.
        '''
        id = MAVLINK_MSG_ID_PARAM_REQUEST_LIST
        name = 'PARAM_REQUEST_LIST'
        fieldnames = ['target_system', 'target_component']
        ordered_fieldnames = [ 'target_system', 'target_component' ]
        format = '<BB'
        native_format = bytearray('<BB', 'ascii')
        orders = [0, 1]
        lengths = [1, 1]
        array_lengths = [0, 0]
        crc_extra = 159

        def __init__(self, target_system, target_component):
                MAVLink_message.__init__(self, MAVLink_param_request_list_message.id, MAVLink_param_request_list_message.name)
                self._fieldnames = MAVLink_param_request_list_message.fieldnames
                self.target_system = target_system
                self.target_component = target_component

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 159, struct.pack('<BB', self.target_system, self.target_component))

class MAVLink_param_value_message(MAVLink_message):
        '''
        Emit the value of a onboard parameter. The inclusion of
        param_count and param_index in the message allows the
        recipient to keep track of received parameters and allows him
        to re-request missing parameters after a loss or timeout.
        '''
        id = MAVLINK_MSG_ID_PARAM_VALUE
        name = 'PARAM_VALUE'
        fieldnames = ['param_id', 'param_value', 'param_type', 'param_count', 'param_index']
        ordered_fieldnames = [ 'param_value', 'param_count', 'param_index', 'param_id', 'param_type' ]
        format = '<fHH16sB'
        native_format = bytearray('<fHHcB', 'ascii')
        orders = [3, 0, 4, 1, 2]
        lengths = [1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 16, 0]
        crc_extra = 220

        def __init__(self, param_id, param_value, param_type, param_count, param_index):
                MAVLink_message.__init__(self, MAVLink_param_value_message.id, MAVLink_param_value_message.name)
                self._fieldnames = MAVLink_param_value_message.fieldnames
                self.param_id = param_id
                self.param_value = param_value
                self.param_type = param_type
                self.param_count = param_count
                self.param_index = param_index

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 220, struct.pack('<fHH16sB', self.param_value, self.param_count, self.param_index, self.param_id, self.param_type))

class MAVLink_param_set_message(MAVLink_message):
        '''
        Set a parameter value TEMPORARILY to RAM. It will be reset to
        default on system reboot. Send the ACTION
        MAV_ACTION_STORAGE_WRITE to PERMANENTLY write the RAM contents
        to EEPROM. IMPORTANT: The receiving component should
        acknowledge the new parameter value by sending a param_value
        message to all communication partners. This will also ensure
        that multiple GCS all have an up-to-date list of all
        parameters. If the sending GCS did not receive a PARAM_VALUE
        message within its timeout time, it should re-send the
        PARAM_SET message.
        '''
        id = MAVLINK_MSG_ID_PARAM_SET
        name = 'PARAM_SET'
        fieldnames = ['target_system', 'target_component', 'param_id', 'param_value', 'param_type']
        ordered_fieldnames = [ 'param_value', 'target_system', 'target_component', 'param_id', 'param_type' ]
        format = '<fBB16sB'
        native_format = bytearray('<fBBcB', 'ascii')
        orders = [1, 2, 3, 0, 4]
        lengths = [1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 16, 0]
        crc_extra = 168

        def __init__(self, target_system, target_component, param_id, param_value, param_type):
                MAVLink_message.__init__(self, MAVLink_param_set_message.id, MAVLink_param_set_message.name)
                self._fieldnames = MAVLink_param_set_message.fieldnames
                self.target_system = target_system
                self.target_component = target_component
                self.param_id = param_id
                self.param_value = param_value
                self.param_type = param_type

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 168, struct.pack('<fBB16sB', self.param_value, self.target_system, self.target_component, self.param_id, self.param_type))

class MAVLink_gps_raw_int_message(MAVLink_message):
        '''
        The global position, as returned by the Global Positioning
        System (GPS). This is                 NOT the global position
        estimate of the system, but rather a RAW sensor value. See
        message GLOBAL_POSITION for the global position estimate.
        Coordinate frame is right-handed, Z-axis up (GPS frame).
        '''
        id = MAVLINK_MSG_ID_GPS_RAW_INT
        name = 'GPS_RAW_INT'
        fieldnames = ['time_usec', 'fix_type', 'lat', 'lon', 'alt', 'eph', 'epv', 'vel', 'cog', 'satellites_visible']
        ordered_fieldnames = [ 'time_usec', 'lat', 'lon', 'alt', 'eph', 'epv', 'vel', 'cog', 'fix_type', 'satellites_visible' ]
        format = '<QiiiHHHHBB'
        native_format = bytearray('<QiiiHHHHBB', 'ascii')
        orders = [0, 8, 1, 2, 3, 4, 5, 6, 7, 9]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 24

        def __init__(self, time_usec, fix_type, lat, lon, alt, eph, epv, vel, cog, satellites_visible):
                MAVLink_message.__init__(self, MAVLink_gps_raw_int_message.id, MAVLink_gps_raw_int_message.name)
                self._fieldnames = MAVLink_gps_raw_int_message.fieldnames
                self.time_usec = time_usec
                self.fix_type = fix_type
                self.lat = lat
                self.lon = lon
                self.alt = alt
                self.eph = eph
                self.epv = epv
                self.vel = vel
                self.cog = cog
                self.satellites_visible = satellites_visible

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 24, struct.pack('<QiiiHHHHBB', self.time_usec, self.lat, self.lon, self.alt, self.eph, self.epv, self.vel, self.cog, self.fix_type, self.satellites_visible))

class MAVLink_gps_status_message(MAVLink_message):
        '''
        The positioning status, as reported by GPS. This message is
        intended to display status information about each satellite
        visible to the receiver. See message GLOBAL_POSITION for the
        global position estimate. This message can contain information
        for up to 20 satellites.
        '''
        id = MAVLINK_MSG_ID_GPS_STATUS
        name = 'GPS_STATUS'
        fieldnames = ['satellites_visible', 'satellite_prn', 'satellite_used', 'satellite_elevation', 'satellite_azimuth', 'satellite_snr']
        ordered_fieldnames = [ 'satellites_visible', 'satellite_prn', 'satellite_used', 'satellite_elevation', 'satellite_azimuth', 'satellite_snr' ]
        format = '<B20B20B20B20B20B'
        native_format = bytearray('<BBBBBB', 'ascii')
        orders = [0, 1, 2, 3, 4, 5]
        lengths = [1, 20, 20, 20, 20, 20]
        array_lengths = [0, 20, 20, 20, 20, 20]
        crc_extra = 23

        def __init__(self, satellites_visible, satellite_prn, satellite_used, satellite_elevation, satellite_azimuth, satellite_snr):
                MAVLink_message.__init__(self, MAVLink_gps_status_message.id, MAVLink_gps_status_message.name)
                self._fieldnames = MAVLink_gps_status_message.fieldnames
                self.satellites_visible = satellites_visible
                self.satellite_prn = satellite_prn
                self.satellite_used = satellite_used
                self.satellite_elevation = satellite_elevation
                self.satellite_azimuth = satellite_azimuth
                self.satellite_snr = satellite_snr

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 23, struct.pack('<B20B20B20B20B20B', self.satellites_visible, self.satellite_prn[0], self.satellite_prn[1], self.satellite_prn[2], self.satellite_prn[3], self.satellite_prn[4], self.satellite_prn[5], self.satellite_prn[6], self.satellite_prn[7], self.satellite_prn[8], self.satellite_prn[9], self.satellite_prn[10], self.satellite_prn[11], self.satellite_prn[12], self.satellite_prn[13], self.satellite_prn[14], self.satellite_prn[15], self.satellite_prn[16], self.satellite_prn[17], self.satellite_prn[18], self.satellite_prn[19], self.satellite_used[0], self.satellite_used[1], self.satellite_used[2], self.satellite_used[3], self.satellite_used[4], self.satellite_used[5], self.satellite_used[6], self.satellite_used[7], self.satellite_used[8], self.satellite_used[9], self.satellite_used[10], self.satellite_used[11], self.satellite_used[12], self.satellite_used[13], self.satellite_used[14], self.satellite_used[15], self.satellite_used[16], self.satellite_used[17], self.satellite_used[18], self.satellite_used[19], self.satellite_elevation[0], self.satellite_elevation[1], self.satellite_elevation[2], self.satellite_elevation[3], self.satellite_elevation[4], self.satellite_elevation[5], self.satellite_elevation[6], self.satellite_elevation[7], self.satellite_elevation[8], self.satellite_elevation[9], self.satellite_elevation[10], self.satellite_elevation[11], self.satellite_elevation[12], self.satellite_elevation[13], self.satellite_elevation[14], self.satellite_elevation[15], self.satellite_elevation[16], self.satellite_elevation[17], self.satellite_elevation[18], self.satellite_elevation[19], self.satellite_azimuth[0], self.satellite_azimuth[1], self.satellite_azimuth[2], self.satellite_azimuth[3], self.satellite_azimuth[4], self.satellite_azimuth[5], self.satellite_azimuth[6], self.satellite_azimuth[7], self.satellite_azimuth[8], self.satellite_azimuth[9], self.satellite_azimuth[10], self.satellite_azimuth[11], self.satellite_azimuth[12], self.satellite_azimuth[13], self.satellite_azimuth[14], self.satellite_azimuth[15], self.satellite_azimuth[16], self.satellite_azimuth[17], self.satellite_azimuth[18], self.satellite_azimuth[19], self.satellite_snr[0], self.satellite_snr[1], self.satellite_snr[2], self.satellite_snr[3], self.satellite_snr[4], self.satellite_snr[5], self.satellite_snr[6], self.satellite_snr[7], self.satellite_snr[8], self.satellite_snr[9], self.satellite_snr[10], self.satellite_snr[11], self.satellite_snr[12], self.satellite_snr[13], self.satellite_snr[14], self.satellite_snr[15], self.satellite_snr[16], self.satellite_snr[17], self.satellite_snr[18], self.satellite_snr[19]))

class MAVLink_scaled_imu_message(MAVLink_message):
        '''
        The RAW IMU readings for the usual 9DOF sensor setup. This
        message should contain the scaled values to the described
        units
        '''
        id = MAVLINK_MSG_ID_SCALED_IMU
        name = 'SCALED_IMU'
        fieldnames = ['time_boot_ms', 'xacc', 'yacc', 'zacc', 'xgyro', 'ygyro', 'zgyro', 'xmag', 'ymag', 'zmag']
        ordered_fieldnames = [ 'time_boot_ms', 'xacc', 'yacc', 'zacc', 'xgyro', 'ygyro', 'zgyro', 'xmag', 'ymag', 'zmag' ]
        format = '<Ihhhhhhhhh'
        native_format = bytearray('<Ihhhhhhhhh', 'ascii')
        orders = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 170

        def __init__(self, time_boot_ms, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag):
                MAVLink_message.__init__(self, MAVLink_scaled_imu_message.id, MAVLink_scaled_imu_message.name)
                self._fieldnames = MAVLink_scaled_imu_message.fieldnames
                self.time_boot_ms = time_boot_ms
                self.xacc = xacc
                self.yacc = yacc
                self.zacc = zacc
                self.xgyro = xgyro
                self.ygyro = ygyro
                self.zgyro = zgyro
                self.xmag = xmag
                self.ymag = ymag
                self.zmag = zmag

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 170, struct.pack('<Ihhhhhhhhh', self.time_boot_ms, self.xacc, self.yacc, self.zacc, self.xgyro, self.ygyro, self.zgyro, self.xmag, self.ymag, self.zmag))

class MAVLink_raw_imu_message(MAVLink_message):
        '''
        The RAW IMU readings for the usual 9DOF sensor setup. This
        message should always contain the true raw values without any
        scaling to allow data capture and system debugging.
        '''
        id = MAVLINK_MSG_ID_RAW_IMU
        name = 'RAW_IMU'
        fieldnames = ['time_usec', 'xacc', 'yacc', 'zacc', 'xgyro', 'ygyro', 'zgyro', 'xmag', 'ymag', 'zmag']
        ordered_fieldnames = [ 'time_usec', 'xacc', 'yacc', 'zacc', 'xgyro', 'ygyro', 'zgyro', 'xmag', 'ymag', 'zmag' ]
        format = '<Qhhhhhhhhh'
        native_format = bytearray('<Qhhhhhhhhh', 'ascii')
        orders = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 144

        def __init__(self, time_usec, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag):
                MAVLink_message.__init__(self, MAVLink_raw_imu_message.id, MAVLink_raw_imu_message.name)
                self._fieldnames = MAVLink_raw_imu_message.fieldnames
                self.time_usec = time_usec
                self.xacc = xacc
                self.yacc = yacc
                self.zacc = zacc
                self.xgyro = xgyro
                self.ygyro = ygyro
                self.zgyro = zgyro
                self.xmag = xmag
                self.ymag = ymag
                self.zmag = zmag

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 144, struct.pack('<Qhhhhhhhhh', self.time_usec, self.xacc, self.yacc, self.zacc, self.xgyro, self.ygyro, self.zgyro, self.xmag, self.ymag, self.zmag))

class MAVLink_raw_pressure_message(MAVLink_message):
        '''
        The RAW pressure readings for the typical setup of one
        absolute pressure and one differential pressure sensor. The
        sensor values should be the raw, UNSCALED ADC values.
        '''
        id = MAVLINK_MSG_ID_RAW_PRESSURE
        name = 'RAW_PRESSURE'
        fieldnames = ['time_usec', 'press_abs', 'press_diff1', 'press_diff2', 'temperature']
        ordered_fieldnames = [ 'time_usec', 'press_abs', 'press_diff1', 'press_diff2', 'temperature' ]
        format = '<Qhhhh'
        native_format = bytearray('<Qhhhh', 'ascii')
        orders = [0, 1, 2, 3, 4]
        lengths = [1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0]
        crc_extra = 67

        def __init__(self, time_usec, press_abs, press_diff1, press_diff2, temperature):
                MAVLink_message.__init__(self, MAVLink_raw_pressure_message.id, MAVLink_raw_pressure_message.name)
                self._fieldnames = MAVLink_raw_pressure_message.fieldnames
                self.time_usec = time_usec
                self.press_abs = press_abs
                self.press_diff1 = press_diff1
                self.press_diff2 = press_diff2
                self.temperature = temperature

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 67, struct.pack('<Qhhhh', self.time_usec, self.press_abs, self.press_diff1, self.press_diff2, self.temperature))

class MAVLink_scaled_pressure_message(MAVLink_message):
        '''
        The pressure readings for the typical setup of one absolute
        and differential pressure sensor. The units are as specified
        in each field.
        '''
        id = MAVLINK_MSG_ID_SCALED_PRESSURE
        name = 'SCALED_PRESSURE'
        fieldnames = ['time_boot_ms', 'press_abs', 'press_diff', 'temperature']
        ordered_fieldnames = [ 'time_boot_ms', 'press_abs', 'press_diff', 'temperature' ]
        format = '<Iffh'
        native_format = bytearray('<Iffh', 'ascii')
        orders = [0, 1, 2, 3]
        lengths = [1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0]
        crc_extra = 115

        def __init__(self, time_boot_ms, press_abs, press_diff, temperature):
                MAVLink_message.__init__(self, MAVLink_scaled_pressure_message.id, MAVLink_scaled_pressure_message.name)
                self._fieldnames = MAVLink_scaled_pressure_message.fieldnames
                self.time_boot_ms = time_boot_ms
                self.press_abs = press_abs
                self.press_diff = press_diff
                self.temperature = temperature

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 115, struct.pack('<Iffh', self.time_boot_ms, self.press_abs, self.press_diff, self.temperature))

class MAVLink_attitude_message(MAVLink_message):
        '''
        The attitude in the aeronautical frame (right-handed, Z-down,
        X-front, Y-right).
        '''
        id = MAVLINK_MSG_ID_ATTITUDE
        name = 'ATTITUDE'
        fieldnames = ['time_boot_ms', 'roll', 'pitch', 'yaw', 'rollspeed', 'pitchspeed', 'yawspeed']
        ordered_fieldnames = [ 'time_boot_ms', 'roll', 'pitch', 'yaw', 'rollspeed', 'pitchspeed', 'yawspeed' ]
        format = '<Iffffff'
        native_format = bytearray('<Iffffff', 'ascii')
        orders = [0, 1, 2, 3, 4, 5, 6]
        lengths = [1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0]
        crc_extra = 39

        def __init__(self, time_boot_ms, roll, pitch, yaw, rollspeed, pitchspeed, yawspeed):
                MAVLink_message.__init__(self, MAVLink_attitude_message.id, MAVLink_attitude_message.name)
                self._fieldnames = MAVLink_attitude_message.fieldnames
                self.time_boot_ms = time_boot_ms
                self.roll = roll
                self.pitch = pitch
                self.yaw = yaw
                self.rollspeed = rollspeed
                self.pitchspeed = pitchspeed
                self.yawspeed = yawspeed

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 39, struct.pack('<Iffffff', self.time_boot_ms, self.roll, self.pitch, self.yaw, self.rollspeed, self.pitchspeed, self.yawspeed))

class MAVLink_attitude_quaternion_message(MAVLink_message):
        '''
        The attitude in the aeronautical frame (right-handed, Z-down,
        X-front, Y-right), expressed as quaternion. Quaternion order
        is w, x, y, z and a zero rotation would be expressed as (1 0 0
        0).
        '''
        id = MAVLINK_MSG_ID_ATTITUDE_QUATERNION
        name = 'ATTITUDE_QUATERNION'
        fieldnames = ['time_boot_ms', 'q1', 'q2', 'q3', 'q4', 'rollspeed', 'pitchspeed', 'yawspeed']
        ordered_fieldnames = [ 'time_boot_ms', 'q1', 'q2', 'q3', 'q4', 'rollspeed', 'pitchspeed', 'yawspeed' ]
        format = '<Ifffffff'
        native_format = bytearray('<Ifffffff', 'ascii')
        orders = [0, 1, 2, 3, 4, 5, 6, 7]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 246

        def __init__(self, time_boot_ms, q1, q2, q3, q4, rollspeed, pitchspeed, yawspeed):
                MAVLink_message.__init__(self, MAVLink_attitude_quaternion_message.id, MAVLink_attitude_quaternion_message.name)
                self._fieldnames = MAVLink_attitude_quaternion_message.fieldnames
                self.time_boot_ms = time_boot_ms
                self.q1 = q1
                self.q2 = q2
                self.q3 = q3
                self.q4 = q4
                self.rollspeed = rollspeed
                self.pitchspeed = pitchspeed
                self.yawspeed = yawspeed

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 246, struct.pack('<Ifffffff', self.time_boot_ms, self.q1, self.q2, self.q3, self.q4, self.rollspeed, self.pitchspeed, self.yawspeed))

class MAVLink_local_position_ned_message(MAVLink_message):
        '''
        The filtered local position (e.g. fused computer vision and
        accelerometers). Coordinate frame is right-handed, Z-axis down
        (aeronautical frame, NED / north-east-down convention)
        '''
        id = MAVLINK_MSG_ID_LOCAL_POSITION_NED
        name = 'LOCAL_POSITION_NED'
        fieldnames = ['time_boot_ms', 'x', 'y', 'z', 'vx', 'vy', 'vz']
        ordered_fieldnames = [ 'time_boot_ms', 'x', 'y', 'z', 'vx', 'vy', 'vz' ]
        format = '<Iffffff'
        native_format = bytearray('<Iffffff', 'ascii')
        orders = [0, 1, 2, 3, 4, 5, 6]
        lengths = [1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0]
        crc_extra = 185

        def __init__(self, time_boot_ms, x, y, z, vx, vy, vz):
                MAVLink_message.__init__(self, MAVLink_local_position_ned_message.id, MAVLink_local_position_ned_message.name)
                self._fieldnames = MAVLink_local_position_ned_message.fieldnames
                self.time_boot_ms = time_boot_ms
                self.x = x
                self.y = y
                self.z = z
                self.vx = vx
                self.vy = vy
                self.vz = vz

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 185, struct.pack('<Iffffff', self.time_boot_ms, self.x, self.y, self.z, self.vx, self.vy, self.vz))

class MAVLink_global_position_int_message(MAVLink_message):
        '''
        The filtered global position (e.g. fused GPS and
        accelerometers). The position is in GPS-frame (right-handed,
        Z-up). It                is designed as scaled integer message
        since the resolution of float is not sufficient.
        '''
        id = MAVLINK_MSG_ID_GLOBAL_POSITION_INT
        name = 'GLOBAL_POSITION_INT'
        fieldnames = ['time_boot_ms', 'lat', 'lon', 'alt', 'relative_alt', 'vx', 'vy', 'vz', 'hdg']
        ordered_fieldnames = [ 'time_boot_ms', 'lat', 'lon', 'alt', 'relative_alt', 'vx', 'vy', 'vz', 'hdg' ]
        format = '<IiiiihhhH'
        native_format = bytearray('<IiiiihhhH', 'ascii')
        orders = [0, 1, 2, 3, 4, 5, 6, 7, 8]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 104

        def __init__(self, time_boot_ms, lat, lon, alt, relative_alt, vx, vy, vz, hdg):
                MAVLink_message.__init__(self, MAVLink_global_position_int_message.id, MAVLink_global_position_int_message.name)
                self._fieldnames = MAVLink_global_position_int_message.fieldnames
                self.time_boot_ms = time_boot_ms
                self.lat = lat
                self.lon = lon
                self.alt = alt
                self.relative_alt = relative_alt
                self.vx = vx
                self.vy = vy
                self.vz = vz
                self.hdg = hdg

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 104, struct.pack('<IiiiihhhH', self.time_boot_ms, self.lat, self.lon, self.alt, self.relative_alt, self.vx, self.vy, self.vz, self.hdg))

class MAVLink_rc_channels_scaled_message(MAVLink_message):
        '''
        The scaled values of the RC channels received. (-100%) -10000,
        (0%) 0, (100%) 10000. Channels that are inactive should be set
        to UINT16_MAX.
        '''
        id = MAVLINK_MSG_ID_RC_CHANNELS_SCALED
        name = 'RC_CHANNELS_SCALED'
        fieldnames = ['time_boot_ms', 'port', 'chan1_scaled', 'chan2_scaled', 'chan3_scaled', 'chan4_scaled', 'chan5_scaled', 'chan6_scaled', 'chan7_scaled', 'chan8_scaled', 'rssi']
        ordered_fieldnames = [ 'time_boot_ms', 'chan1_scaled', 'chan2_scaled', 'chan3_scaled', 'chan4_scaled', 'chan5_scaled', 'chan6_scaled', 'chan7_scaled', 'chan8_scaled', 'port', 'rssi' ]
        format = '<IhhhhhhhhBB'
        native_format = bytearray('<IhhhhhhhhBB', 'ascii')
        orders = [0, 9, 1, 2, 3, 4, 5, 6, 7, 8, 10]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 237

        def __init__(self, time_boot_ms, port, chan1_scaled, chan2_scaled, chan3_scaled, chan4_scaled, chan5_scaled, chan6_scaled, chan7_scaled, chan8_scaled, rssi):
                MAVLink_message.__init__(self, MAVLink_rc_channels_scaled_message.id, MAVLink_rc_channels_scaled_message.name)
                self._fieldnames = MAVLink_rc_channels_scaled_message.fieldnames
                self.time_boot_ms = time_boot_ms
                self.port = port
                self.chan1_scaled = chan1_scaled
                self.chan2_scaled = chan2_scaled
                self.chan3_scaled = chan3_scaled
                self.chan4_scaled = chan4_scaled
                self.chan5_scaled = chan5_scaled
                self.chan6_scaled = chan6_scaled
                self.chan7_scaled = chan7_scaled
                self.chan8_scaled = chan8_scaled
                self.rssi = rssi

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 237, struct.pack('<IhhhhhhhhBB', self.time_boot_ms, self.chan1_scaled, self.chan2_scaled, self.chan3_scaled, self.chan4_scaled, self.chan5_scaled, self.chan6_scaled, self.chan7_scaled, self.chan8_scaled, self.port, self.rssi))

class MAVLink_rc_channels_raw_message(MAVLink_message):
        '''
        The RAW values of the RC channels received. The standard PPM
        modulation is as follows: 1000 microseconds: 0%, 2000
        microseconds: 100%. Individual receivers/transmitters might
        violate this specification.
        '''
        id = MAVLINK_MSG_ID_RC_CHANNELS_RAW
        name = 'RC_CHANNELS_RAW'
        fieldnames = ['time_boot_ms', 'port', 'chan1_raw', 'chan2_raw', 'chan3_raw', 'chan4_raw', 'chan5_raw', 'chan6_raw', 'chan7_raw', 'chan8_raw', 'rssi']
        ordered_fieldnames = [ 'time_boot_ms', 'chan1_raw', 'chan2_raw', 'chan3_raw', 'chan4_raw', 'chan5_raw', 'chan6_raw', 'chan7_raw', 'chan8_raw', 'port', 'rssi' ]
        format = '<IHHHHHHHHBB'
        native_format = bytearray('<IHHHHHHHHBB', 'ascii')
        orders = [0, 9, 1, 2, 3, 4, 5, 6, 7, 8, 10]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 244

        def __init__(self, time_boot_ms, port, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw, rssi):
                MAVLink_message.__init__(self, MAVLink_rc_channels_raw_message.id, MAVLink_rc_channels_raw_message.name)
                self._fieldnames = MAVLink_rc_channels_raw_message.fieldnames
                self.time_boot_ms = time_boot_ms
                self.port = port
                self.chan1_raw = chan1_raw
                self.chan2_raw = chan2_raw
                self.chan3_raw = chan3_raw
                self.chan4_raw = chan4_raw
                self.chan5_raw = chan5_raw
                self.chan6_raw = chan6_raw
                self.chan7_raw = chan7_raw
                self.chan8_raw = chan8_raw
                self.rssi = rssi

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 244, struct.pack('<IHHHHHHHHBB', self.time_boot_ms, self.chan1_raw, self.chan2_raw, self.chan3_raw, self.chan4_raw, self.chan5_raw, self.chan6_raw, self.chan7_raw, self.chan8_raw, self.port, self.rssi))

class MAVLink_servo_output_raw_message(MAVLink_message):
        '''
        The RAW values of the servo outputs (for RC input from the
        remote, use the RC_CHANNELS messages). The standard PPM
        modulation is as follows: 1000 microseconds: 0%, 2000
        microseconds: 100%.
        '''
        id = MAVLINK_MSG_ID_SERVO_OUTPUT_RAW
        name = 'SERVO_OUTPUT_RAW'
        fieldnames = ['time_usec', 'port', 'servo1_raw', 'servo2_raw', 'servo3_raw', 'servo4_raw', 'servo5_raw', 'servo6_raw', 'servo7_raw', 'servo8_raw']
        ordered_fieldnames = [ 'time_usec', 'servo1_raw', 'servo2_raw', 'servo3_raw', 'servo4_raw', 'servo5_raw', 'servo6_raw', 'servo7_raw', 'servo8_raw', 'port' ]
        format = '<IHHHHHHHHB'
        native_format = bytearray('<IHHHHHHHHB', 'ascii')
        orders = [0, 9, 1, 2, 3, 4, 5, 6, 7, 8]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 222

        def __init__(self, time_usec, port, servo1_raw, servo2_raw, servo3_raw, servo4_raw, servo5_raw, servo6_raw, servo7_raw, servo8_raw):
                MAVLink_message.__init__(self, MAVLink_servo_output_raw_message.id, MAVLink_servo_output_raw_message.name)
                self._fieldnames = MAVLink_servo_output_raw_message.fieldnames
                self.time_usec = time_usec
                self.port = port
                self.servo1_raw = servo1_raw
                self.servo2_raw = servo2_raw
                self.servo3_raw = servo3_raw
                self.servo4_raw = servo4_raw
                self.servo5_raw = servo5_raw
                self.servo6_raw = servo6_raw
                self.servo7_raw = servo7_raw
                self.servo8_raw = servo8_raw

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 222, struct.pack('<IHHHHHHHHB', self.time_usec, self.servo1_raw, self.servo2_raw, self.servo3_raw, self.servo4_raw, self.servo5_raw, self.servo6_raw, self.servo7_raw, self.servo8_raw, self.port))

class MAVLink_mission_request_partial_list_message(MAVLink_message):
        '''
        Request a partial list of mission items from the
        system/component.
        http://qgroundcontrol.org/mavlink/waypoint_protocol. If start
        and end index are the same, just send one waypoint.
        '''
        id = MAVLINK_MSG_ID_MISSION_REQUEST_PARTIAL_LIST
        name = 'MISSION_REQUEST_PARTIAL_LIST'
        fieldnames = ['target_system', 'target_component', 'start_index', 'end_index']
        ordered_fieldnames = [ 'start_index', 'end_index', 'target_system', 'target_component' ]
        format = '<hhBB'
        native_format = bytearray('<hhBB', 'ascii')
        orders = [2, 3, 0, 1]
        lengths = [1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0]
        crc_extra = 212

        def __init__(self, target_system, target_component, start_index, end_index):
                MAVLink_message.__init__(self, MAVLink_mission_request_partial_list_message.id, MAVLink_mission_request_partial_list_message.name)
                self._fieldnames = MAVLink_mission_request_partial_list_message.fieldnames
                self.target_system = target_system
                self.target_component = target_component
                self.start_index = start_index
                self.end_index = end_index

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 212, struct.pack('<hhBB', self.start_index, self.end_index, self.target_system, self.target_component))

class MAVLink_mission_write_partial_list_message(MAVLink_message):
        '''
        This message is sent to the MAV to write a partial list. If
        start index == end index, only one item will be transmitted /
        updated. If the start index is NOT 0 and above the current
        list size, this request should be REJECTED!
        '''
        id = MAVLINK_MSG_ID_MISSION_WRITE_PARTIAL_LIST
        name = 'MISSION_WRITE_PARTIAL_LIST'
        fieldnames = ['target_system', 'target_component', 'start_index', 'end_index']
        ordered_fieldnames = [ 'start_index', 'end_index', 'target_system', 'target_component' ]
        format = '<hhBB'
        native_format = bytearray('<hhBB', 'ascii')
        orders = [2, 3, 0, 1]
        lengths = [1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0]
        crc_extra = 9

        def __init__(self, target_system, target_component, start_index, end_index):
                MAVLink_message.__init__(self, MAVLink_mission_write_partial_list_message.id, MAVLink_mission_write_partial_list_message.name)
                self._fieldnames = MAVLink_mission_write_partial_list_message.fieldnames
                self.target_system = target_system
                self.target_component = target_component
                self.start_index = start_index
                self.end_index = end_index

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 9, struct.pack('<hhBB', self.start_index, self.end_index, self.target_system, self.target_component))

class MAVLink_mission_item_message(MAVLink_message):
        '''
        Message encoding a mission item. This message is emitted to
        announce                 the presence of a mission item and to
        set a mission item on the system. The mission item can be
        either in x, y, z meters (type: LOCAL) or x:lat, y:lon,
        z:altitude. Local frame is Z-down, right handed (NED), global
        frame is Z-up, right handed (ENU). See also
        http://qgroundcontrol.org/mavlink/waypoint_protocol.
        '''
        id = MAVLINK_MSG_ID_MISSION_ITEM
        name = 'MISSION_ITEM'
        fieldnames = ['target_system', 'target_component', 'seq', 'frame', 'command', 'current', 'autocontinue', 'param1', 'param2', 'param3', 'param4', 'x', 'y', 'z']
        ordered_fieldnames = [ 'param1', 'param2', 'param3', 'param4', 'x', 'y', 'z', 'seq', 'command', 'target_system', 'target_component', 'frame', 'current', 'autocontinue' ]
        format = '<fffffffHHBBBBB'
        native_format = bytearray('<fffffffHHBBBBB', 'ascii')
        orders = [9, 10, 7, 11, 8, 12, 13, 0, 1, 2, 3, 4, 5, 6]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 254

        def __init__(self, target_system, target_component, seq, frame, command, current, autocontinue, param1, param2, param3, param4, x, y, z):
                MAVLink_message.__init__(self, MAVLink_mission_item_message.id, MAVLink_mission_item_message.name)
                self._fieldnames = MAVLink_mission_item_message.fieldnames
                self.target_system = target_system
                self.target_component = target_component
                self.seq = seq
                self.frame = frame
                self.command = command
                self.current = current
                self.autocontinue = autocontinue
                self.param1 = param1
                self.param2 = param2
                self.param3 = param3
                self.param4 = param4
                self.x = x
                self.y = y
                self.z = z

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 254, struct.pack('<fffffffHHBBBBB', self.param1, self.param2, self.param3, self.param4, self.x, self.y, self.z, self.seq, self.command, self.target_system, self.target_component, self.frame, self.current, self.autocontinue))

class MAVLink_mission_request_message(MAVLink_message):
        '''
        Request the information of the mission item with the sequence
        number seq. The response of the system to this message should
        be a MISSION_ITEM message.
        http://qgroundcontrol.org/mavlink/waypoint_protocol
        '''
        id = MAVLINK_MSG_ID_MISSION_REQUEST
        name = 'MISSION_REQUEST'
        fieldnames = ['target_system', 'target_component', 'seq']
        ordered_fieldnames = [ 'seq', 'target_system', 'target_component' ]
        format = '<HBB'
        native_format = bytearray('<HBB', 'ascii')
        orders = [1, 2, 0]
        lengths = [1, 1, 1]
        array_lengths = [0, 0, 0]
        crc_extra = 230

        def __init__(self, target_system, target_component, seq):
                MAVLink_message.__init__(self, MAVLink_mission_request_message.id, MAVLink_mission_request_message.name)
                self._fieldnames = MAVLink_mission_request_message.fieldnames
                self.target_system = target_system
                self.target_component = target_component
                self.seq = seq

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 230, struct.pack('<HBB', self.seq, self.target_system, self.target_component))

class MAVLink_mission_set_current_message(MAVLink_message):
        '''
        Set the mission item with sequence number seq as current item.
        This means that the MAV will continue to this mission item on
        the shortest path (not following the mission items in-
        between).
        '''
        id = MAVLINK_MSG_ID_MISSION_SET_CURRENT
        name = 'MISSION_SET_CURRENT'
        fieldnames = ['target_system', 'target_component', 'seq']
        ordered_fieldnames = [ 'seq', 'target_system', 'target_component' ]
        format = '<HBB'
        native_format = bytearray('<HBB', 'ascii')
        orders = [1, 2, 0]
        lengths = [1, 1, 1]
        array_lengths = [0, 0, 0]
        crc_extra = 28

        def __init__(self, target_system, target_component, seq):
                MAVLink_message.__init__(self, MAVLink_mission_set_current_message.id, MAVLink_mission_set_current_message.name)
                self._fieldnames = MAVLink_mission_set_current_message.fieldnames
                self.target_system = target_system
                self.target_component = target_component
                self.seq = seq

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 28, struct.pack('<HBB', self.seq, self.target_system, self.target_component))

class MAVLink_mission_current_message(MAVLink_message):
        '''
        Message that announces the sequence number of the current
        active mission item. The MAV will fly towards this mission
        item.
        '''
        id = MAVLINK_MSG_ID_MISSION_CURRENT
        name = 'MISSION_CURRENT'
        fieldnames = ['seq']
        ordered_fieldnames = [ 'seq' ]
        format = '<H'
        native_format = bytearray('<H', 'ascii')
        orders = [0]
        lengths = [1]
        array_lengths = [0]
        crc_extra = 28

        def __init__(self, seq):
                MAVLink_message.__init__(self, MAVLink_mission_current_message.id, MAVLink_mission_current_message.name)
                self._fieldnames = MAVLink_mission_current_message.fieldnames
                self.seq = seq

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 28, struct.pack('<H', self.seq))

class MAVLink_mission_request_list_message(MAVLink_message):
        '''
        Request the overall list of mission items from the
        system/component.
        '''
        id = MAVLINK_MSG_ID_MISSION_REQUEST_LIST
        name = 'MISSION_REQUEST_LIST'
        fieldnames = ['target_system', 'target_component']
        ordered_fieldnames = [ 'target_system', 'target_component' ]
        format = '<BB'
        native_format = bytearray('<BB', 'ascii')
        orders = [0, 1]
        lengths = [1, 1]
        array_lengths = [0, 0]
        crc_extra = 132

        def __init__(self, target_system, target_component):
                MAVLink_message.__init__(self, MAVLink_mission_request_list_message.id, MAVLink_mission_request_list_message.name)
                self._fieldnames = MAVLink_mission_request_list_message.fieldnames
                self.target_system = target_system
                self.target_component = target_component

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 132, struct.pack('<BB', self.target_system, self.target_component))

class MAVLink_mission_count_message(MAVLink_message):
        '''
        This message is emitted as response to MISSION_REQUEST_LIST by
        the MAV and to initiate a write transaction. The GCS can then
        request the individual mission item based on the knowledge of
        the total number of MISSIONs.
        '''
        id = MAVLINK_MSG_ID_MISSION_COUNT
        name = 'MISSION_COUNT'
        fieldnames = ['target_system', 'target_component', 'count']
        ordered_fieldnames = [ 'count', 'target_system', 'target_component' ]
        format = '<HBB'
        native_format = bytearray('<HBB', 'ascii')
        orders = [1, 2, 0]
        lengths = [1, 1, 1]
        array_lengths = [0, 0, 0]
        crc_extra = 221

        def __init__(self, target_system, target_component, count):
                MAVLink_message.__init__(self, MAVLink_mission_count_message.id, MAVLink_mission_count_message.name)
                self._fieldnames = MAVLink_mission_count_message.fieldnames
                self.target_system = target_system
                self.target_component = target_component
                self.count = count

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 221, struct.pack('<HBB', self.count, self.target_system, self.target_component))

class MAVLink_mission_clear_all_message(MAVLink_message):
        '''
        Delete all mission items at once.
        '''
        id = MAVLINK_MSG_ID_MISSION_CLEAR_ALL
        name = 'MISSION_CLEAR_ALL'
        fieldnames = ['target_system', 'target_component']
        ordered_fieldnames = [ 'target_system', 'target_component' ]
        format = '<BB'
        native_format = bytearray('<BB', 'ascii')
        orders = [0, 1]
        lengths = [1, 1]
        array_lengths = [0, 0]
        crc_extra = 232

        def __init__(self, target_system, target_component):
                MAVLink_message.__init__(self, MAVLink_mission_clear_all_message.id, MAVLink_mission_clear_all_message.name)
                self._fieldnames = MAVLink_mission_clear_all_message.fieldnames
                self.target_system = target_system
                self.target_component = target_component

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 232, struct.pack('<BB', self.target_system, self.target_component))

class MAVLink_mission_item_reached_message(MAVLink_message):
        '''
        A certain mission item has been reached. The system will
        either hold this position (or circle on the orbit) or (if the
        autocontinue on the WP was set) continue to the next MISSION.
        '''
        id = MAVLINK_MSG_ID_MISSION_ITEM_REACHED
        name = 'MISSION_ITEM_REACHED'
        fieldnames = ['seq']
        ordered_fieldnames = [ 'seq' ]
        format = '<H'
        native_format = bytearray('<H', 'ascii')
        orders = [0]
        lengths = [1]
        array_lengths = [0]
        crc_extra = 11

        def __init__(self, seq):
                MAVLink_message.__init__(self, MAVLink_mission_item_reached_message.id, MAVLink_mission_item_reached_message.name)
                self._fieldnames = MAVLink_mission_item_reached_message.fieldnames
                self.seq = seq

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 11, struct.pack('<H', self.seq))

class MAVLink_mission_ack_message(MAVLink_message):
        '''
        Ack message during MISSION handling. The type field states if
        this message is a positive ack (type=0) or if an error
        happened (type=non-zero).
        '''
        id = MAVLINK_MSG_ID_MISSION_ACK
        name = 'MISSION_ACK'
        fieldnames = ['target_system', 'target_component', 'type']
        ordered_fieldnames = [ 'target_system', 'target_component', 'type' ]
        format = '<BBB'
        native_format = bytearray('<BBB', 'ascii')
        orders = [0, 1, 2]
        lengths = [1, 1, 1]
        array_lengths = [0, 0, 0]
        crc_extra = 153

        def __init__(self, target_system, target_component, type):
                MAVLink_message.__init__(self, MAVLink_mission_ack_message.id, MAVLink_mission_ack_message.name)
                self._fieldnames = MAVLink_mission_ack_message.fieldnames
                self.target_system = target_system
                self.target_component = target_component
                self.type = type

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 153, struct.pack('<BBB', self.target_system, self.target_component, self.type))

class MAVLink_set_gps_global_origin_message(MAVLink_message):
        '''
        As local waypoints exist, the global MISSION reference allows
        to transform between the local coordinate frame and the global
        (GPS) coordinate frame. This can be necessary when e.g. in-
        and outdoor settings are connected and the MAV should move
        from in- to outdoor.
        '''
        id = MAVLINK_MSG_ID_SET_GPS_GLOBAL_ORIGIN
        name = 'SET_GPS_GLOBAL_ORIGIN'
        fieldnames = ['target_system', 'latitude', 'longitude', 'altitude']
        ordered_fieldnames = [ 'latitude', 'longitude', 'altitude', 'target_system' ]
        format = '<iiiB'
        native_format = bytearray('<iiiB', 'ascii')
        orders = [3, 0, 1, 2]
        lengths = [1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0]
        crc_extra = 41

        def __init__(self, target_system, latitude, longitude, altitude):
                MAVLink_message.__init__(self, MAVLink_set_gps_global_origin_message.id, MAVLink_set_gps_global_origin_message.name)
                self._fieldnames = MAVLink_set_gps_global_origin_message.fieldnames
                self.target_system = target_system
                self.latitude = latitude
                self.longitude = longitude
                self.altitude = altitude

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 41, struct.pack('<iiiB', self.latitude, self.longitude, self.altitude, self.target_system))

class MAVLink_gps_global_origin_message(MAVLink_message):
        '''
        Once the MAV sets a new GPS-Local correspondence, this message
        announces the origin (0,0,0) position
        '''
        id = MAVLINK_MSG_ID_GPS_GLOBAL_ORIGIN
        name = 'GPS_GLOBAL_ORIGIN'
        fieldnames = ['latitude', 'longitude', 'altitude']
        ordered_fieldnames = [ 'latitude', 'longitude', 'altitude' ]
        format = '<iii'
        native_format = bytearray('<iii', 'ascii')
        orders = [0, 1, 2]
        lengths = [1, 1, 1]
        array_lengths = [0, 0, 0]
        crc_extra = 39

        def __init__(self, latitude, longitude, altitude):
                MAVLink_message.__init__(self, MAVLink_gps_global_origin_message.id, MAVLink_gps_global_origin_message.name)
                self._fieldnames = MAVLink_gps_global_origin_message.fieldnames
                self.latitude = latitude
                self.longitude = longitude
                self.altitude = altitude

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 39, struct.pack('<iii', self.latitude, self.longitude, self.altitude))

class MAVLink_param_map_rc_message(MAVLink_message):
        '''
        Bind a RC channel to a parameter. The parameter should change
        accoding to the RC channel value.
        '''
        id = MAVLINK_MSG_ID_PARAM_MAP_RC
        name = 'PARAM_MAP_RC'
        fieldnames = ['target_system', 'target_component', 'param_id', 'param_index', 'parameter_rc_channel_index', 'param_value0', 'scale', 'param_value_min', 'param_value_max']
        ordered_fieldnames = [ 'param_value0', 'scale', 'param_value_min', 'param_value_max', 'param_index', 'target_system', 'target_component', 'param_id', 'parameter_rc_channel_index' ]
        format = '<ffffhBB16sB'
        native_format = bytearray('<ffffhBBcB', 'ascii')
        orders = [5, 6, 7, 4, 8, 0, 1, 2, 3]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 16, 0]
        crc_extra = 78

        def __init__(self, target_system, target_component, param_id, param_index, parameter_rc_channel_index, param_value0, scale, param_value_min, param_value_max):
                MAVLink_message.__init__(self, MAVLink_param_map_rc_message.id, MAVLink_param_map_rc_message.name)
                self._fieldnames = MAVLink_param_map_rc_message.fieldnames
                self.target_system = target_system
                self.target_component = target_component
                self.param_id = param_id
                self.param_index = param_index
                self.parameter_rc_channel_index = parameter_rc_channel_index
                self.param_value0 = param_value0
                self.scale = scale
                self.param_value_min = param_value_min
                self.param_value_max = param_value_max

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 78, struct.pack('<ffffhBB16sB', self.param_value0, self.scale, self.param_value_min, self.param_value_max, self.param_index, self.target_system, self.target_component, self.param_id, self.parameter_rc_channel_index))

class MAVLink_safety_set_allowed_area_message(MAVLink_message):
        '''
        Set a safety zone (volume), which is defined by two corners of
        a cube. This message can be used to tell the MAV which
        setpoints/MISSIONs to accept and which to reject. Safety areas
        are often enforced by national or competition regulations.
        '''
        id = MAVLINK_MSG_ID_SAFETY_SET_ALLOWED_AREA
        name = 'SAFETY_SET_ALLOWED_AREA'
        fieldnames = ['target_system', 'target_component', 'frame', 'p1x', 'p1y', 'p1z', 'p2x', 'p2y', 'p2z']
        ordered_fieldnames = [ 'p1x', 'p1y', 'p1z', 'p2x', 'p2y', 'p2z', 'target_system', 'target_component', 'frame' ]
        format = '<ffffffBBB'
        native_format = bytearray('<ffffffBBB', 'ascii')
        orders = [6, 7, 8, 0, 1, 2, 3, 4, 5]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 15

        def __init__(self, target_system, target_component, frame, p1x, p1y, p1z, p2x, p2y, p2z):
                MAVLink_message.__init__(self, MAVLink_safety_set_allowed_area_message.id, MAVLink_safety_set_allowed_area_message.name)
                self._fieldnames = MAVLink_safety_set_allowed_area_message.fieldnames
                self.target_system = target_system
                self.target_component = target_component
                self.frame = frame
                self.p1x = p1x
                self.p1y = p1y
                self.p1z = p1z
                self.p2x = p2x
                self.p2y = p2y
                self.p2z = p2z

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 15, struct.pack('<ffffffBBB', self.p1x, self.p1y, self.p1z, self.p2x, self.p2y, self.p2z, self.target_system, self.target_component, self.frame))

class MAVLink_safety_allowed_area_message(MAVLink_message):
        '''
        Read out the safety zone the MAV currently assumes.
        '''
        id = MAVLINK_MSG_ID_SAFETY_ALLOWED_AREA
        name = 'SAFETY_ALLOWED_AREA'
        fieldnames = ['frame', 'p1x', 'p1y', 'p1z', 'p2x', 'p2y', 'p2z']
        ordered_fieldnames = [ 'p1x', 'p1y', 'p1z', 'p2x', 'p2y', 'p2z', 'frame' ]
        format = '<ffffffB'
        native_format = bytearray('<ffffffB', 'ascii')
        orders = [6, 0, 1, 2, 3, 4, 5]
        lengths = [1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0]
        crc_extra = 3

        def __init__(self, frame, p1x, p1y, p1z, p2x, p2y, p2z):
                MAVLink_message.__init__(self, MAVLink_safety_allowed_area_message.id, MAVLink_safety_allowed_area_message.name)
                self._fieldnames = MAVLink_safety_allowed_area_message.fieldnames
                self.frame = frame
                self.p1x = p1x
                self.p1y = p1y
                self.p1z = p1z
                self.p2x = p2x
                self.p2y = p2y
                self.p2z = p2z

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 3, struct.pack('<ffffffB', self.p1x, self.p1y, self.p1z, self.p2x, self.p2y, self.p2z, self.frame))

class MAVLink_attitude_quaternion_cov_message(MAVLink_message):
        '''
        The attitude in the aeronautical frame (right-handed, Z-down,
        X-front, Y-right), expressed as quaternion. Quaternion order
        is w, x, y, z and a zero rotation would be expressed as (1 0 0
        0).
        '''
        id = MAVLINK_MSG_ID_ATTITUDE_QUATERNION_COV
        name = 'ATTITUDE_QUATERNION_COV'
        fieldnames = ['time_boot_ms', 'q', 'rollspeed', 'pitchspeed', 'yawspeed', 'covariance']
        ordered_fieldnames = [ 'time_boot_ms', 'q', 'rollspeed', 'pitchspeed', 'yawspeed', 'covariance' ]
        format = '<I4ffff9f'
        native_format = bytearray('<Ifffff', 'ascii')
        orders = [0, 1, 2, 3, 4, 5]
        lengths = [1, 4, 1, 1, 1, 9]
        array_lengths = [0, 4, 0, 0, 0, 9]
        crc_extra = 153

        def __init__(self, time_boot_ms, q, rollspeed, pitchspeed, yawspeed, covariance):
                MAVLink_message.__init__(self, MAVLink_attitude_quaternion_cov_message.id, MAVLink_attitude_quaternion_cov_message.name)
                self._fieldnames = MAVLink_attitude_quaternion_cov_message.fieldnames
                self.time_boot_ms = time_boot_ms
                self.q = q
                self.rollspeed = rollspeed
                self.pitchspeed = pitchspeed
                self.yawspeed = yawspeed
                self.covariance = covariance

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 153, struct.pack('<I4ffff9f', self.time_boot_ms, self.q[0], self.q[1], self.q[2], self.q[3], self.rollspeed, self.pitchspeed, self.yawspeed, self.covariance[0], self.covariance[1], self.covariance[2], self.covariance[3], self.covariance[4], self.covariance[5], self.covariance[6], self.covariance[7], self.covariance[8]))

class MAVLink_nav_controller_output_message(MAVLink_message):
        '''
        Outputs of the APM navigation controller. The primary use of
        this message is to check the response and signs of the
        controller before actual flight and to assist with tuning
        controller parameters.
        '''
        id = MAVLINK_MSG_ID_NAV_CONTROLLER_OUTPUT
        name = 'NAV_CONTROLLER_OUTPUT'
        fieldnames = ['nav_roll', 'nav_pitch', 'nav_bearing', 'target_bearing', 'wp_dist', 'alt_error', 'aspd_error', 'xtrack_error']
        ordered_fieldnames = [ 'nav_roll', 'nav_pitch', 'alt_error', 'aspd_error', 'xtrack_error', 'nav_bearing', 'target_bearing', 'wp_dist' ]
        format = '<fffffhhH'
        native_format = bytearray('<fffffhhH', 'ascii')
        orders = [0, 1, 5, 6, 7, 2, 3, 4]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 183

        def __init__(self, nav_roll, nav_pitch, nav_bearing, target_bearing, wp_dist, alt_error, aspd_error, xtrack_error):
                MAVLink_message.__init__(self, MAVLink_nav_controller_output_message.id, MAVLink_nav_controller_output_message.name)
                self._fieldnames = MAVLink_nav_controller_output_message.fieldnames
                self.nav_roll = nav_roll
                self.nav_pitch = nav_pitch
                self.nav_bearing = nav_bearing
                self.target_bearing = target_bearing
                self.wp_dist = wp_dist
                self.alt_error = alt_error
                self.aspd_error = aspd_error
                self.xtrack_error = xtrack_error

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 183, struct.pack('<fffffhhH', self.nav_roll, self.nav_pitch, self.alt_error, self.aspd_error, self.xtrack_error, self.nav_bearing, self.target_bearing, self.wp_dist))

class MAVLink_global_position_int_cov_message(MAVLink_message):
        '''
        The filtered global position (e.g. fused GPS and
        accelerometers). The position is in GPS-frame (right-handed,
        Z-up). It  is designed as scaled integer message since the
        resolution of float is not sufficient. NOTE: This message is
        intended for onboard networks / companion computers and
        higher-bandwidth links and optimized for accuracy and
        completeness. Please use the GLOBAL_POSITION_INT message for a
        minimal subset.
        '''
        id = MAVLINK_MSG_ID_GLOBAL_POSITION_INT_COV
        name = 'GLOBAL_POSITION_INT_COV'
        fieldnames = ['time_boot_ms', 'time_utc', 'estimator_type', 'lat', 'lon', 'alt', 'relative_alt', 'vx', 'vy', 'vz', 'covariance']
        ordered_fieldnames = [ 'time_utc', 'time_boot_ms', 'lat', 'lon', 'alt', 'relative_alt', 'vx', 'vy', 'vz', 'covariance', 'estimator_type' ]
        format = '<QIiiiifff36fB'
        native_format = bytearray('<QIiiiiffffB', 'ascii')
        orders = [1, 0, 10, 2, 3, 4, 5, 6, 7, 8, 9]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 36, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 36, 0]
        crc_extra = 51

        def __init__(self, time_boot_ms, time_utc, estimator_type, lat, lon, alt, relative_alt, vx, vy, vz, covariance):
                MAVLink_message.__init__(self, MAVLink_global_position_int_cov_message.id, MAVLink_global_position_int_cov_message.name)
                self._fieldnames = MAVLink_global_position_int_cov_message.fieldnames
                self.time_boot_ms = time_boot_ms
                self.time_utc = time_utc
                self.estimator_type = estimator_type
                self.lat = lat
                self.lon = lon
                self.alt = alt
                self.relative_alt = relative_alt
                self.vx = vx
                self.vy = vy
                self.vz = vz
                self.covariance = covariance

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 51, struct.pack('<QIiiiifff36fB', self.time_utc, self.time_boot_ms, self.lat, self.lon, self.alt, self.relative_alt, self.vx, self.vy, self.vz, self.covariance[0], self.covariance[1], self.covariance[2], self.covariance[3], self.covariance[4], self.covariance[5], self.covariance[6], self.covariance[7], self.covariance[8], self.covariance[9], self.covariance[10], self.covariance[11], self.covariance[12], self.covariance[13], self.covariance[14], self.covariance[15], self.covariance[16], self.covariance[17], self.covariance[18], self.covariance[19], self.covariance[20], self.covariance[21], self.covariance[22], self.covariance[23], self.covariance[24], self.covariance[25], self.covariance[26], self.covariance[27], self.covariance[28], self.covariance[29], self.covariance[30], self.covariance[31], self.covariance[32], self.covariance[33], self.covariance[34], self.covariance[35], self.estimator_type))

class MAVLink_local_position_ned_cov_message(MAVLink_message):
        '''
        The filtered local position (e.g. fused computer vision and
        accelerometers). Coordinate frame is right-handed, Z-axis down
        (aeronautical frame, NED / north-east-down convention)
        '''
        id = MAVLINK_MSG_ID_LOCAL_POSITION_NED_COV
        name = 'LOCAL_POSITION_NED_COV'
        fieldnames = ['time_boot_ms', 'time_utc', 'estimator_type', 'x', 'y', 'z', 'vx', 'vy', 'vz', 'ax', 'ay', 'az', 'covariance']
        ordered_fieldnames = [ 'time_utc', 'time_boot_ms', 'x', 'y', 'z', 'vx', 'vy', 'vz', 'ax', 'ay', 'az', 'covariance', 'estimator_type' ]
        format = '<QIfffffffff45fB'
        native_format = bytearray('<QIffffffffffB', 'ascii')
        orders = [1, 0, 12, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 45, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 45, 0]
        crc_extra = 59

        def __init__(self, time_boot_ms, time_utc, estimator_type, x, y, z, vx, vy, vz, ax, ay, az, covariance):
                MAVLink_message.__init__(self, MAVLink_local_position_ned_cov_message.id, MAVLink_local_position_ned_cov_message.name)
                self._fieldnames = MAVLink_local_position_ned_cov_message.fieldnames
                self.time_boot_ms = time_boot_ms
                self.time_utc = time_utc
                self.estimator_type = estimator_type
                self.x = x
                self.y = y
                self.z = z
                self.vx = vx
                self.vy = vy
                self.vz = vz
                self.ax = ax
                self.ay = ay
                self.az = az
                self.covariance = covariance

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 59, struct.pack('<QIfffffffff45fB', self.time_utc, self.time_boot_ms, self.x, self.y, self.z, self.vx, self.vy, self.vz, self.ax, self.ay, self.az, self.covariance[0], self.covariance[1], self.covariance[2], self.covariance[3], self.covariance[4], self.covariance[5], self.covariance[6], self.covariance[7], self.covariance[8], self.covariance[9], self.covariance[10], self.covariance[11], self.covariance[12], self.covariance[13], self.covariance[14], self.covariance[15], self.covariance[16], self.covariance[17], self.covariance[18], self.covariance[19], self.covariance[20], self.covariance[21], self.covariance[22], self.covariance[23], self.covariance[24], self.covariance[25], self.covariance[26], self.covariance[27], self.covariance[28], self.covariance[29], self.covariance[30], self.covariance[31], self.covariance[32], self.covariance[33], self.covariance[34], self.covariance[35], self.covariance[36], self.covariance[37], self.covariance[38], self.covariance[39], self.covariance[40], self.covariance[41], self.covariance[42], self.covariance[43], self.covariance[44], self.estimator_type))

class MAVLink_rc_channels_message(MAVLink_message):
        '''
        The PPM values of the RC channels received. The standard PPM
        modulation is as follows: 1000 microseconds: 0%, 2000
        microseconds: 100%. Individual receivers/transmitters might
        violate this specification.
        '''
        id = MAVLINK_MSG_ID_RC_CHANNELS
        name = 'RC_CHANNELS'
        fieldnames = ['time_boot_ms', 'chancount', 'chan1_raw', 'chan2_raw', 'chan3_raw', 'chan4_raw', 'chan5_raw', 'chan6_raw', 'chan7_raw', 'chan8_raw', 'chan9_raw', 'chan10_raw', 'chan11_raw', 'chan12_raw', 'chan13_raw', 'chan14_raw', 'chan15_raw', 'chan16_raw', 'chan17_raw', 'chan18_raw', 'rssi']
        ordered_fieldnames = [ 'time_boot_ms', 'chan1_raw', 'chan2_raw', 'chan3_raw', 'chan4_raw', 'chan5_raw', 'chan6_raw', 'chan7_raw', 'chan8_raw', 'chan9_raw', 'chan10_raw', 'chan11_raw', 'chan12_raw', 'chan13_raw', 'chan14_raw', 'chan15_raw', 'chan16_raw', 'chan17_raw', 'chan18_raw', 'chancount', 'rssi' ]
        format = '<IHHHHHHHHHHHHHHHHHHBB'
        native_format = bytearray('<IHHHHHHHHHHHHHHHHHHBB', 'ascii')
        orders = [0, 19, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 20]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 118

        def __init__(self, time_boot_ms, chancount, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw, chan9_raw, chan10_raw, chan11_raw, chan12_raw, chan13_raw, chan14_raw, chan15_raw, chan16_raw, chan17_raw, chan18_raw, rssi):
                MAVLink_message.__init__(self, MAVLink_rc_channels_message.id, MAVLink_rc_channels_message.name)
                self._fieldnames = MAVLink_rc_channels_message.fieldnames
                self.time_boot_ms = time_boot_ms
                self.chancount = chancount
                self.chan1_raw = chan1_raw
                self.chan2_raw = chan2_raw
                self.chan3_raw = chan3_raw
                self.chan4_raw = chan4_raw
                self.chan5_raw = chan5_raw
                self.chan6_raw = chan6_raw
                self.chan7_raw = chan7_raw
                self.chan8_raw = chan8_raw
                self.chan9_raw = chan9_raw
                self.chan10_raw = chan10_raw
                self.chan11_raw = chan11_raw
                self.chan12_raw = chan12_raw
                self.chan13_raw = chan13_raw
                self.chan14_raw = chan14_raw
                self.chan15_raw = chan15_raw
                self.chan16_raw = chan16_raw
                self.chan17_raw = chan17_raw
                self.chan18_raw = chan18_raw
                self.rssi = rssi

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 118, struct.pack('<IHHHHHHHHHHHHHHHHHHBB', self.time_boot_ms, self.chan1_raw, self.chan2_raw, self.chan3_raw, self.chan4_raw, self.chan5_raw, self.chan6_raw, self.chan7_raw, self.chan8_raw, self.chan9_raw, self.chan10_raw, self.chan11_raw, self.chan12_raw, self.chan13_raw, self.chan14_raw, self.chan15_raw, self.chan16_raw, self.chan17_raw, self.chan18_raw, self.chancount, self.rssi))

class MAVLink_request_data_stream_message(MAVLink_message):
        '''

        '''
        id = MAVLINK_MSG_ID_REQUEST_DATA_STREAM
        name = 'REQUEST_DATA_STREAM'
        fieldnames = ['target_system', 'target_component', 'req_stream_id', 'req_message_rate', 'start_stop']
        ordered_fieldnames = [ 'req_message_rate', 'target_system', 'target_component', 'req_stream_id', 'start_stop' ]
        format = '<HBBBB'
        native_format = bytearray('<HBBBB', 'ascii')
        orders = [1, 2, 3, 0, 4]
        lengths = [1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0]
        crc_extra = 148

        def __init__(self, target_system, target_component, req_stream_id, req_message_rate, start_stop):
                MAVLink_message.__init__(self, MAVLink_request_data_stream_message.id, MAVLink_request_data_stream_message.name)
                self._fieldnames = MAVLink_request_data_stream_message.fieldnames
                self.target_system = target_system
                self.target_component = target_component
                self.req_stream_id = req_stream_id
                self.req_message_rate = req_message_rate
                self.start_stop = start_stop

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 148, struct.pack('<HBBBB', self.req_message_rate, self.target_system, self.target_component, self.req_stream_id, self.start_stop))

class MAVLink_data_stream_message(MAVLink_message):
        '''

        '''
        id = MAVLINK_MSG_ID_DATA_STREAM
        name = 'DATA_STREAM'
        fieldnames = ['stream_id', 'message_rate', 'on_off']
        ordered_fieldnames = [ 'message_rate', 'stream_id', 'on_off' ]
        format = '<HBB'
        native_format = bytearray('<HBB', 'ascii')
        orders = [1, 0, 2]
        lengths = [1, 1, 1]
        array_lengths = [0, 0, 0]
        crc_extra = 21

        def __init__(self, stream_id, message_rate, on_off):
                MAVLink_message.__init__(self, MAVLink_data_stream_message.id, MAVLink_data_stream_message.name)
                self._fieldnames = MAVLink_data_stream_message.fieldnames
                self.stream_id = stream_id
                self.message_rate = message_rate
                self.on_off = on_off

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 21, struct.pack('<HBB', self.message_rate, self.stream_id, self.on_off))

class MAVLink_manual_control_message(MAVLink_message):
        '''
        This message provides an API for manually controlling the
        vehicle using standard joystick axes nomenclature, along with
        a joystick-like input device. Unused axes can be disabled an
        buttons are also transmit as boolean values of their
        '''
        id = MAVLINK_MSG_ID_MANUAL_CONTROL
        name = 'MANUAL_CONTROL'
        fieldnames = ['target', 'x', 'y', 'z', 'r', 'buttons']
        ordered_fieldnames = [ 'x', 'y', 'z', 'r', 'buttons', 'target' ]
        format = '<hhhhHB'
        native_format = bytearray('<hhhhHB', 'ascii')
        orders = [5, 0, 1, 2, 3, 4]
        lengths = [1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0]
        crc_extra = 243

        def __init__(self, target, x, y, z, r, buttons):
                MAVLink_message.__init__(self, MAVLink_manual_control_message.id, MAVLink_manual_control_message.name)
                self._fieldnames = MAVLink_manual_control_message.fieldnames
                self.target = target
                self.x = x
                self.y = y
                self.z = z
                self.r = r
                self.buttons = buttons

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 243, struct.pack('<hhhhHB', self.x, self.y, self.z, self.r, self.buttons, self.target))

class MAVLink_rc_channels_override_message(MAVLink_message):
        '''
        The RAW values of the RC channels sent to the MAV to override
        info received from the RC radio. A value of UINT16_MAX means
        no change to that channel. A value of 0 means control of that
        channel should be released back to the RC radio. The standard
        PPM modulation is as follows: 1000 microseconds: 0%, 2000
        microseconds: 100%. Individual receivers/transmitters might
        violate this specification.
        '''
        id = MAVLINK_MSG_ID_RC_CHANNELS_OVERRIDE
        name = 'RC_CHANNELS_OVERRIDE'
        fieldnames = ['target_system', 'target_component', 'chan1_raw', 'chan2_raw', 'chan3_raw', 'chan4_raw', 'chan5_raw', 'chan6_raw', 'chan7_raw', 'chan8_raw']
        ordered_fieldnames = [ 'chan1_raw', 'chan2_raw', 'chan3_raw', 'chan4_raw', 'chan5_raw', 'chan6_raw', 'chan7_raw', 'chan8_raw', 'target_system', 'target_component' ]
        format = '<HHHHHHHHBB'
        native_format = bytearray('<HHHHHHHHBB', 'ascii')
        orders = [8, 9, 0, 1, 2, 3, 4, 5, 6, 7]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 124

        def __init__(self, target_system, target_component, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw):
                MAVLink_message.__init__(self, MAVLink_rc_channels_override_message.id, MAVLink_rc_channels_override_message.name)
                self._fieldnames = MAVLink_rc_channels_override_message.fieldnames
                self.target_system = target_system
                self.target_component = target_component
                self.chan1_raw = chan1_raw
                self.chan2_raw = chan2_raw
                self.chan3_raw = chan3_raw
                self.chan4_raw = chan4_raw
                self.chan5_raw = chan5_raw
                self.chan6_raw = chan6_raw
                self.chan7_raw = chan7_raw
                self.chan8_raw = chan8_raw

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 124, struct.pack('<HHHHHHHHBB', self.chan1_raw, self.chan2_raw, self.chan3_raw, self.chan4_raw, self.chan5_raw, self.chan6_raw, self.chan7_raw, self.chan8_raw, self.target_system, self.target_component))

class MAVLink_mission_item_int_message(MAVLink_message):
        '''
        Message encoding a mission item. This message is emitted to
        announce                 the presence of a mission item and to
        set a mission item on the system. The mission item can be
        either in x, y, z meters (type: LOCAL) or x:lat, y:lon,
        z:altitude. Local frame is Z-down, right handed (NED), global
        frame is Z-up, right handed (ENU). See
        alsohttp://qgroundcontrol.org/mavlink/waypoint_protocol.
        '''
        id = MAVLINK_MSG_ID_MISSION_ITEM_INT
        name = 'MISSION_ITEM_INT'
        fieldnames = ['target_system', 'target_component', 'seq', 'frame', 'command', 'current', 'autocontinue', 'param1', 'param2', 'param3', 'param4', 'x', 'y', 'z']
        ordered_fieldnames = [ 'param1', 'param2', 'param3', 'param4', 'x', 'y', 'z', 'seq', 'command', 'target_system', 'target_component', 'frame', 'current', 'autocontinue' ]
        format = '<ffffiifHHBBBBB'
        native_format = bytearray('<ffffiifHHBBBBB', 'ascii')
        orders = [9, 10, 7, 11, 8, 12, 13, 0, 1, 2, 3, 4, 5, 6]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 38

        def __init__(self, target_system, target_component, seq, frame, command, current, autocontinue, param1, param2, param3, param4, x, y, z):
                MAVLink_message.__init__(self, MAVLink_mission_item_int_message.id, MAVLink_mission_item_int_message.name)
                self._fieldnames = MAVLink_mission_item_int_message.fieldnames
                self.target_system = target_system
                self.target_component = target_component
                self.seq = seq
                self.frame = frame
                self.command = command
                self.current = current
                self.autocontinue = autocontinue
                self.param1 = param1
                self.param2 = param2
                self.param3 = param3
                self.param4 = param4
                self.x = x
                self.y = y
                self.z = z

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 38, struct.pack('<ffffiifHHBBBBB', self.param1, self.param2, self.param3, self.param4, self.x, self.y, self.z, self.seq, self.command, self.target_system, self.target_component, self.frame, self.current, self.autocontinue))

class MAVLink_vfr_hud_message(MAVLink_message):
        '''
        Metrics typically displayed on a HUD for fixed wing aircraft
        '''
        id = MAVLINK_MSG_ID_VFR_HUD
        name = 'VFR_HUD'
        fieldnames = ['airspeed', 'groundspeed', 'heading', 'throttle', 'alt', 'climb']
        ordered_fieldnames = [ 'airspeed', 'groundspeed', 'alt', 'climb', 'heading', 'throttle' ]
        format = '<ffffhH'
        native_format = bytearray('<ffffhH', 'ascii')
        orders = [0, 1, 4, 5, 2, 3]
        lengths = [1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0]
        crc_extra = 20

        def __init__(self, airspeed, groundspeed, heading, throttle, alt, climb):
                MAVLink_message.__init__(self, MAVLink_vfr_hud_message.id, MAVLink_vfr_hud_message.name)
                self._fieldnames = MAVLink_vfr_hud_message.fieldnames
                self.airspeed = airspeed
                self.groundspeed = groundspeed
                self.heading = heading
                self.throttle = throttle
                self.alt = alt
                self.climb = climb

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 20, struct.pack('<ffffhH', self.airspeed, self.groundspeed, self.alt, self.climb, self.heading, self.throttle))

class MAVLink_command_int_message(MAVLink_message):
        '''
        Message encoding a command with parameters as scaled integers.
        Scaling depends on the actual command value.
        '''
        id = MAVLINK_MSG_ID_COMMAND_INT
        name = 'COMMAND_INT'
        fieldnames = ['target_system', 'target_component', 'frame', 'command', 'current', 'autocontinue', 'param1', 'param2', 'param3', 'param4', 'x', 'y', 'z']
        ordered_fieldnames = [ 'param1', 'param2', 'param3', 'param4', 'x', 'y', 'z', 'command', 'target_system', 'target_component', 'frame', 'current', 'autocontinue' ]
        format = '<ffffiifHBBBBB'
        native_format = bytearray('<ffffiifHBBBBB', 'ascii')
        orders = [8, 9, 10, 7, 11, 12, 0, 1, 2, 3, 4, 5, 6]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 158

        def __init__(self, target_system, target_component, frame, command, current, autocontinue, param1, param2, param3, param4, x, y, z):
                MAVLink_message.__init__(self, MAVLink_command_int_message.id, MAVLink_command_int_message.name)
                self._fieldnames = MAVLink_command_int_message.fieldnames
                self.target_system = target_system
                self.target_component = target_component
                self.frame = frame
                self.command = command
                self.current = current
                self.autocontinue = autocontinue
                self.param1 = param1
                self.param2 = param2
                self.param3 = param3
                self.param4 = param4
                self.x = x
                self.y = y
                self.z = z

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 158, struct.pack('<ffffiifHBBBBB', self.param1, self.param2, self.param3, self.param4, self.x, self.y, self.z, self.command, self.target_system, self.target_component, self.frame, self.current, self.autocontinue))

class MAVLink_command_long_message(MAVLink_message):
        '''
        Send a command with up to seven parameters to the MAV
        '''
        id = MAVLINK_MSG_ID_COMMAND_LONG
        name = 'COMMAND_LONG'
        fieldnames = ['target_system', 'target_component', 'command', 'confirmation', 'param1', 'param2', 'param3', 'param4', 'param5', 'param6', 'param7']
        ordered_fieldnames = [ 'param1', 'param2', 'param3', 'param4', 'param5', 'param6', 'param7', 'command', 'target_system', 'target_component', 'confirmation' ]
        format = '<fffffffHBBB'
        native_format = bytearray('<fffffffHBBB', 'ascii')
        orders = [8, 9, 7, 10, 0, 1, 2, 3, 4, 5, 6]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 152

        def __init__(self, target_system, target_component, command, confirmation, param1, param2, param3, param4, param5, param6, param7):
                MAVLink_message.__init__(self, MAVLink_command_long_message.id, MAVLink_command_long_message.name)
                self._fieldnames = MAVLink_command_long_message.fieldnames
                self.target_system = target_system
                self.target_component = target_component
                self.command = command
                self.confirmation = confirmation
                self.param1 = param1
                self.param2 = param2
                self.param3 = param3
                self.param4 = param4
                self.param5 = param5
                self.param6 = param6
                self.param7 = param7

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 152, struct.pack('<fffffffHBBB', self.param1, self.param2, self.param3, self.param4, self.param5, self.param6, self.param7, self.command, self.target_system, self.target_component, self.confirmation))

class MAVLink_command_ack_message(MAVLink_message):
        '''
        Report status of a command. Includes feedback wether the
        command was executed.
        '''
        id = MAVLINK_MSG_ID_COMMAND_ACK
        name = 'COMMAND_ACK'
        fieldnames = ['command', 'result']
        ordered_fieldnames = [ 'command', 'result' ]
        format = '<HB'
        native_format = bytearray('<HB', 'ascii')
        orders = [0, 1]
        lengths = [1, 1]
        array_lengths = [0, 0]
        crc_extra = 143

        def __init__(self, command, result):
                MAVLink_message.__init__(self, MAVLink_command_ack_message.id, MAVLink_command_ack_message.name)
                self._fieldnames = MAVLink_command_ack_message.fieldnames
                self.command = command
                self.result = result

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 143, struct.pack('<HB', self.command, self.result))

class MAVLink_manual_setpoint_message(MAVLink_message):
        '''
        Setpoint in roll, pitch, yaw and thrust from the operator
        '''
        id = MAVLINK_MSG_ID_MANUAL_SETPOINT
        name = 'MANUAL_SETPOINT'
        fieldnames = ['time_boot_ms', 'roll', 'pitch', 'yaw', 'thrust', 'mode_switch', 'manual_override_switch']
        ordered_fieldnames = [ 'time_boot_ms', 'roll', 'pitch', 'yaw', 'thrust', 'mode_switch', 'manual_override_switch' ]
        format = '<IffffBB'
        native_format = bytearray('<IffffBB', 'ascii')
        orders = [0, 1, 2, 3, 4, 5, 6]
        lengths = [1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0]
        crc_extra = 106

        def __init__(self, time_boot_ms, roll, pitch, yaw, thrust, mode_switch, manual_override_switch):
                MAVLink_message.__init__(self, MAVLink_manual_setpoint_message.id, MAVLink_manual_setpoint_message.name)
                self._fieldnames = MAVLink_manual_setpoint_message.fieldnames
                self.time_boot_ms = time_boot_ms
                self.roll = roll
                self.pitch = pitch
                self.yaw = yaw
                self.thrust = thrust
                self.mode_switch = mode_switch
                self.manual_override_switch = manual_override_switch

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 106, struct.pack('<IffffBB', self.time_boot_ms, self.roll, self.pitch, self.yaw, self.thrust, self.mode_switch, self.manual_override_switch))

class MAVLink_set_attitude_target_message(MAVLink_message):
        '''
        Set the vehicle attitude and body angular rates.
        '''
        id = MAVLINK_MSG_ID_SET_ATTITUDE_TARGET
        name = 'SET_ATTITUDE_TARGET'
        fieldnames = ['time_boot_ms', 'target_system', 'target_component', 'type_mask', 'q', 'body_roll_rate', 'body_pitch_rate', 'body_yaw_rate', 'thrust']
        ordered_fieldnames = [ 'time_boot_ms', 'q', 'body_roll_rate', 'body_pitch_rate', 'body_yaw_rate', 'thrust', 'target_system', 'target_component', 'type_mask' ]
        format = '<I4fffffBBB'
        native_format = bytearray('<IfffffBBB', 'ascii')
        orders = [0, 6, 7, 8, 1, 2, 3, 4, 5]
        lengths = [1, 4, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 4, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 49

        def __init__(self, time_boot_ms, target_system, target_component, type_mask, q, body_roll_rate, body_pitch_rate, body_yaw_rate, thrust):
                MAVLink_message.__init__(self, MAVLink_set_attitude_target_message.id, MAVLink_set_attitude_target_message.name)
                self._fieldnames = MAVLink_set_attitude_target_message.fieldnames
                self.time_boot_ms = time_boot_ms
                self.target_system = target_system
                self.target_component = target_component
                self.type_mask = type_mask
                self.q = q
                self.body_roll_rate = body_roll_rate
                self.body_pitch_rate = body_pitch_rate
                self.body_yaw_rate = body_yaw_rate
                self.thrust = thrust

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 49, struct.pack('<I4fffffBBB', self.time_boot_ms, self.q[0], self.q[1], self.q[2], self.q[3], self.body_roll_rate, self.body_pitch_rate, self.body_yaw_rate, self.thrust, self.target_system, self.target_component, self.type_mask))

class MAVLink_attitude_target_message(MAVLink_message):
        '''
        Set the vehicle attitude and body angular rates.
        '''
        id = MAVLINK_MSG_ID_ATTITUDE_TARGET
        name = 'ATTITUDE_TARGET'
        fieldnames = ['time_boot_ms', 'type_mask', 'q', 'body_roll_rate', 'body_pitch_rate', 'body_yaw_rate', 'thrust']
        ordered_fieldnames = [ 'time_boot_ms', 'q', 'body_roll_rate', 'body_pitch_rate', 'body_yaw_rate', 'thrust', 'type_mask' ]
        format = '<I4fffffB'
        native_format = bytearray('<IfffffB', 'ascii')
        orders = [0, 6, 1, 2, 3, 4, 5]
        lengths = [1, 4, 1, 1, 1, 1, 1]
        array_lengths = [0, 4, 0, 0, 0, 0, 0]
        crc_extra = 22

        def __init__(self, time_boot_ms, type_mask, q, body_roll_rate, body_pitch_rate, body_yaw_rate, thrust):
                MAVLink_message.__init__(self, MAVLink_attitude_target_message.id, MAVLink_attitude_target_message.name)
                self._fieldnames = MAVLink_attitude_target_message.fieldnames
                self.time_boot_ms = time_boot_ms
                self.type_mask = type_mask
                self.q = q
                self.body_roll_rate = body_roll_rate
                self.body_pitch_rate = body_pitch_rate
                self.body_yaw_rate = body_yaw_rate
                self.thrust = thrust

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 22, struct.pack('<I4fffffB', self.time_boot_ms, self.q[0], self.q[1], self.q[2], self.q[3], self.body_roll_rate, self.body_pitch_rate, self.body_yaw_rate, self.thrust, self.type_mask))

class MAVLink_set_position_target_local_ned_message(MAVLink_message):
        '''
        Set vehicle position, velocity and acceleration setpoint in
        local frame.
        '''
        id = MAVLINK_MSG_ID_SET_POSITION_TARGET_LOCAL_NED
        name = 'SET_POSITION_TARGET_LOCAL_NED'
        fieldnames = ['time_boot_ms', 'target_system', 'target_component', 'coordinate_frame', 'type_mask', 'x', 'y', 'z', 'vx', 'vy', 'vz', 'afx', 'afy', 'afz', 'yaw', 'yaw_rate']
        ordered_fieldnames = [ 'time_boot_ms', 'x', 'y', 'z', 'vx', 'vy', 'vz', 'afx', 'afy', 'afz', 'yaw', 'yaw_rate', 'type_mask', 'target_system', 'target_component', 'coordinate_frame' ]
        format = '<IfffffffffffHBBB'
        native_format = bytearray('<IfffffffffffHBBB', 'ascii')
        orders = [0, 13, 14, 15, 12, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 143

        def __init__(self, time_boot_ms, target_system, target_component, coordinate_frame, type_mask, x, y, z, vx, vy, vz, afx, afy, afz, yaw, yaw_rate):
                MAVLink_message.__init__(self, MAVLink_set_position_target_local_ned_message.id, MAVLink_set_position_target_local_ned_message.name)
                self._fieldnames = MAVLink_set_position_target_local_ned_message.fieldnames
                self.time_boot_ms = time_boot_ms
                self.target_system = target_system
                self.target_component = target_component
                self.coordinate_frame = coordinate_frame
                self.type_mask = type_mask
                self.x = x
                self.y = y
                self.z = z
                self.vx = vx
                self.vy = vy
                self.vz = vz
                self.afx = afx
                self.afy = afy
                self.afz = afz
                self.yaw = yaw
                self.yaw_rate = yaw_rate

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 143, struct.pack('<IfffffffffffHBBB', self.time_boot_ms, self.x, self.y, self.z, self.vx, self.vy, self.vz, self.afx, self.afy, self.afz, self.yaw, self.yaw_rate, self.type_mask, self.target_system, self.target_component, self.coordinate_frame))

class MAVLink_position_target_local_ned_message(MAVLink_message):
        '''
        Set vehicle position, velocity and acceleration setpoint in
        local frame.
        '''
        id = MAVLINK_MSG_ID_POSITION_TARGET_LOCAL_NED
        name = 'POSITION_TARGET_LOCAL_NED'
        fieldnames = ['time_boot_ms', 'coordinate_frame', 'type_mask', 'x', 'y', 'z', 'vx', 'vy', 'vz', 'afx', 'afy', 'afz', 'yaw', 'yaw_rate']
        ordered_fieldnames = [ 'time_boot_ms', 'x', 'y', 'z', 'vx', 'vy', 'vz', 'afx', 'afy', 'afz', 'yaw', 'yaw_rate', 'type_mask', 'coordinate_frame' ]
        format = '<IfffffffffffHB'
        native_format = bytearray('<IfffffffffffHB', 'ascii')
        orders = [0, 13, 12, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 140

        def __init__(self, time_boot_ms, coordinate_frame, type_mask, x, y, z, vx, vy, vz, afx, afy, afz, yaw, yaw_rate):
                MAVLink_message.__init__(self, MAVLink_position_target_local_ned_message.id, MAVLink_position_target_local_ned_message.name)
                self._fieldnames = MAVLink_position_target_local_ned_message.fieldnames
                self.time_boot_ms = time_boot_ms
                self.coordinate_frame = coordinate_frame
                self.type_mask = type_mask
                self.x = x
                self.y = y
                self.z = z
                self.vx = vx
                self.vy = vy
                self.vz = vz
                self.afx = afx
                self.afy = afy
                self.afz = afz
                self.yaw = yaw
                self.yaw_rate = yaw_rate

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 140, struct.pack('<IfffffffffffHB', self.time_boot_ms, self.x, self.y, self.z, self.vx, self.vy, self.vz, self.afx, self.afy, self.afz, self.yaw, self.yaw_rate, self.type_mask, self.coordinate_frame))

class MAVLink_set_position_target_global_int_message(MAVLink_message):
        '''
        Set vehicle position, velocity and acceleration setpoint in
        the WGS84 coordinate system.
        '''
        id = MAVLINK_MSG_ID_SET_POSITION_TARGET_GLOBAL_INT
        name = 'SET_POSITION_TARGET_GLOBAL_INT'
        fieldnames = ['time_boot_ms', 'target_system', 'target_component', 'coordinate_frame', 'type_mask', 'lat_int', 'lon_int', 'alt', 'vx', 'vy', 'vz', 'afx', 'afy', 'afz', 'yaw', 'yaw_rate']
        ordered_fieldnames = [ 'time_boot_ms', 'lat_int', 'lon_int', 'alt', 'vx', 'vy', 'vz', 'afx', 'afy', 'afz', 'yaw', 'yaw_rate', 'type_mask', 'target_system', 'target_component', 'coordinate_frame' ]
        format = '<IiifffffffffHBBB'
        native_format = bytearray('<IiifffffffffHBBB', 'ascii')
        orders = [0, 13, 14, 15, 12, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 5

        def __init__(self, time_boot_ms, target_system, target_component, coordinate_frame, type_mask, lat_int, lon_int, alt, vx, vy, vz, afx, afy, afz, yaw, yaw_rate):
                MAVLink_message.__init__(self, MAVLink_set_position_target_global_int_message.id, MAVLink_set_position_target_global_int_message.name)
                self._fieldnames = MAVLink_set_position_target_global_int_message.fieldnames
                self.time_boot_ms = time_boot_ms
                self.target_system = target_system
                self.target_component = target_component
                self.coordinate_frame = coordinate_frame
                self.type_mask = type_mask
                self.lat_int = lat_int
                self.lon_int = lon_int
                self.alt = alt
                self.vx = vx
                self.vy = vy
                self.vz = vz
                self.afx = afx
                self.afy = afy
                self.afz = afz
                self.yaw = yaw
                self.yaw_rate = yaw_rate

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 5, struct.pack('<IiifffffffffHBBB', self.time_boot_ms, self.lat_int, self.lon_int, self.alt, self.vx, self.vy, self.vz, self.afx, self.afy, self.afz, self.yaw, self.yaw_rate, self.type_mask, self.target_system, self.target_component, self.coordinate_frame))

class MAVLink_position_target_global_int_message(MAVLink_message):
        '''
        Set vehicle position, velocity and acceleration setpoint in
        the WGS84 coordinate system.
        '''
        id = MAVLINK_MSG_ID_POSITION_TARGET_GLOBAL_INT
        name = 'POSITION_TARGET_GLOBAL_INT'
        fieldnames = ['time_boot_ms', 'coordinate_frame', 'type_mask', 'lat_int', 'lon_int', 'alt', 'vx', 'vy', 'vz', 'afx', 'afy', 'afz', 'yaw', 'yaw_rate']
        ordered_fieldnames = [ 'time_boot_ms', 'lat_int', 'lon_int', 'alt', 'vx', 'vy', 'vz', 'afx', 'afy', 'afz', 'yaw', 'yaw_rate', 'type_mask', 'coordinate_frame' ]
        format = '<IiifffffffffHB'
        native_format = bytearray('<IiifffffffffHB', 'ascii')
        orders = [0, 13, 12, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 150

        def __init__(self, time_boot_ms, coordinate_frame, type_mask, lat_int, lon_int, alt, vx, vy, vz, afx, afy, afz, yaw, yaw_rate):
                MAVLink_message.__init__(self, MAVLink_position_target_global_int_message.id, MAVLink_position_target_global_int_message.name)
                self._fieldnames = MAVLink_position_target_global_int_message.fieldnames
                self.time_boot_ms = time_boot_ms
                self.coordinate_frame = coordinate_frame
                self.type_mask = type_mask
                self.lat_int = lat_int
                self.lon_int = lon_int
                self.alt = alt
                self.vx = vx
                self.vy = vy
                self.vz = vz
                self.afx = afx
                self.afy = afy
                self.afz = afz
                self.yaw = yaw
                self.yaw_rate = yaw_rate

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 150, struct.pack('<IiifffffffffHB', self.time_boot_ms, self.lat_int, self.lon_int, self.alt, self.vx, self.vy, self.vz, self.afx, self.afy, self.afz, self.yaw, self.yaw_rate, self.type_mask, self.coordinate_frame))

class MAVLink_local_position_ned_system_global_offset_message(MAVLink_message):
        '''
        The offset in X, Y, Z and yaw between the LOCAL_POSITION_NED
        messages of MAV X and the global coordinate frame in NED
        coordinates. Coordinate frame is right-handed, Z-axis down
        (aeronautical frame, NED / north-east-down convention)
        '''
        id = MAVLINK_MSG_ID_LOCAL_POSITION_NED_SYSTEM_GLOBAL_OFFSET
        name = 'LOCAL_POSITION_NED_SYSTEM_GLOBAL_OFFSET'
        fieldnames = ['time_boot_ms', 'x', 'y', 'z', 'roll', 'pitch', 'yaw']
        ordered_fieldnames = [ 'time_boot_ms', 'x', 'y', 'z', 'roll', 'pitch', 'yaw' ]
        format = '<Iffffff'
        native_format = bytearray('<Iffffff', 'ascii')
        orders = [0, 1, 2, 3, 4, 5, 6]
        lengths = [1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0]
        crc_extra = 231

        def __init__(self, time_boot_ms, x, y, z, roll, pitch, yaw):
                MAVLink_message.__init__(self, MAVLink_local_position_ned_system_global_offset_message.id, MAVLink_local_position_ned_system_global_offset_message.name)
                self._fieldnames = MAVLink_local_position_ned_system_global_offset_message.fieldnames
                self.time_boot_ms = time_boot_ms
                self.x = x
                self.y = y
                self.z = z
                self.roll = roll
                self.pitch = pitch
                self.yaw = yaw

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 231, struct.pack('<Iffffff', self.time_boot_ms, self.x, self.y, self.z, self.roll, self.pitch, self.yaw))

class MAVLink_hil_state_message(MAVLink_message):
        '''
        DEPRECATED PACKET! Suffers from missing airspeed fields and
        singularities due to Euler angles. Please use
        HIL_STATE_QUATERNION instead. Sent from simulation to
        autopilot. This packet is useful for high throughput
        applications such as hardware in the loop simulations.
        '''
        id = MAVLINK_MSG_ID_HIL_STATE
        name = 'HIL_STATE'
        fieldnames = ['time_usec', 'roll', 'pitch', 'yaw', 'rollspeed', 'pitchspeed', 'yawspeed', 'lat', 'lon', 'alt', 'vx', 'vy', 'vz', 'xacc', 'yacc', 'zacc']
        ordered_fieldnames = [ 'time_usec', 'roll', 'pitch', 'yaw', 'rollspeed', 'pitchspeed', 'yawspeed', 'lat', 'lon', 'alt', 'vx', 'vy', 'vz', 'xacc', 'yacc', 'zacc' ]
        format = '<Qffffffiiihhhhhh'
        native_format = bytearray('<Qffffffiiihhhhhh', 'ascii')
        orders = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 183

        def __init__(self, time_usec, roll, pitch, yaw, rollspeed, pitchspeed, yawspeed, lat, lon, alt, vx, vy, vz, xacc, yacc, zacc):
                MAVLink_message.__init__(self, MAVLink_hil_state_message.id, MAVLink_hil_state_message.name)
                self._fieldnames = MAVLink_hil_state_message.fieldnames
                self.time_usec = time_usec
                self.roll = roll
                self.pitch = pitch
                self.yaw = yaw
                self.rollspeed = rollspeed
                self.pitchspeed = pitchspeed
                self.yawspeed = yawspeed
                self.lat = lat
                self.lon = lon
                self.alt = alt
                self.vx = vx
                self.vy = vy
                self.vz = vz
                self.xacc = xacc
                self.yacc = yacc
                self.zacc = zacc

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 183, struct.pack('<Qffffffiiihhhhhh', self.time_usec, self.roll, self.pitch, self.yaw, self.rollspeed, self.pitchspeed, self.yawspeed, self.lat, self.lon, self.alt, self.vx, self.vy, self.vz, self.xacc, self.yacc, self.zacc))

class MAVLink_hil_controls_message(MAVLink_message):
        '''
        Sent from autopilot to simulation. Hardware in the loop
        control outputs
        '''
        id = MAVLINK_MSG_ID_HIL_CONTROLS
        name = 'HIL_CONTROLS'
        fieldnames = ['time_usec', 'roll_ailerons', 'pitch_elevator', 'yaw_rudder', 'throttle', 'aux1', 'aux2', 'aux3', 'aux4', 'mode', 'nav_mode']
        ordered_fieldnames = [ 'time_usec', 'roll_ailerons', 'pitch_elevator', 'yaw_rudder', 'throttle', 'aux1', 'aux2', 'aux3', 'aux4', 'mode', 'nav_mode' ]
        format = '<QffffffffBB'
        native_format = bytearray('<QffffffffBB', 'ascii')
        orders = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 63

        def __init__(self, time_usec, roll_ailerons, pitch_elevator, yaw_rudder, throttle, aux1, aux2, aux3, aux4, mode, nav_mode):
                MAVLink_message.__init__(self, MAVLink_hil_controls_message.id, MAVLink_hil_controls_message.name)
                self._fieldnames = MAVLink_hil_controls_message.fieldnames
                self.time_usec = time_usec
                self.roll_ailerons = roll_ailerons
                self.pitch_elevator = pitch_elevator
                self.yaw_rudder = yaw_rudder
                self.throttle = throttle
                self.aux1 = aux1
                self.aux2 = aux2
                self.aux3 = aux3
                self.aux4 = aux4
                self.mode = mode
                self.nav_mode = nav_mode

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 63, struct.pack('<QffffffffBB', self.time_usec, self.roll_ailerons, self.pitch_elevator, self.yaw_rudder, self.throttle, self.aux1, self.aux2, self.aux3, self.aux4, self.mode, self.nav_mode))

class MAVLink_hil_rc_inputs_raw_message(MAVLink_message):
        '''
        Sent from simulation to autopilot. The RAW values of the RC
        channels received. The standard PPM modulation is as follows:
        1000 microseconds: 0%, 2000 microseconds: 100%. Individual
        receivers/transmitters might violate this specification.
        '''
        id = MAVLINK_MSG_ID_HIL_RC_INPUTS_RAW
        name = 'HIL_RC_INPUTS_RAW'
        fieldnames = ['time_usec', 'chan1_raw', 'chan2_raw', 'chan3_raw', 'chan4_raw', 'chan5_raw', 'chan6_raw', 'chan7_raw', 'chan8_raw', 'chan9_raw', 'chan10_raw', 'chan11_raw', 'chan12_raw', 'rssi']
        ordered_fieldnames = [ 'time_usec', 'chan1_raw', 'chan2_raw', 'chan3_raw', 'chan4_raw', 'chan5_raw', 'chan6_raw', 'chan7_raw', 'chan8_raw', 'chan9_raw', 'chan10_raw', 'chan11_raw', 'chan12_raw', 'rssi' ]
        format = '<QHHHHHHHHHHHHB'
        native_format = bytearray('<QHHHHHHHHHHHHB', 'ascii')
        orders = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 54

        def __init__(self, time_usec, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw, chan9_raw, chan10_raw, chan11_raw, chan12_raw, rssi):
                MAVLink_message.__init__(self, MAVLink_hil_rc_inputs_raw_message.id, MAVLink_hil_rc_inputs_raw_message.name)
                self._fieldnames = MAVLink_hil_rc_inputs_raw_message.fieldnames
                self.time_usec = time_usec
                self.chan1_raw = chan1_raw
                self.chan2_raw = chan2_raw
                self.chan3_raw = chan3_raw
                self.chan4_raw = chan4_raw
                self.chan5_raw = chan5_raw
                self.chan6_raw = chan6_raw
                self.chan7_raw = chan7_raw
                self.chan8_raw = chan8_raw
                self.chan9_raw = chan9_raw
                self.chan10_raw = chan10_raw
                self.chan11_raw = chan11_raw
                self.chan12_raw = chan12_raw
                self.rssi = rssi

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 54, struct.pack('<QHHHHHHHHHHHHB', self.time_usec, self.chan1_raw, self.chan2_raw, self.chan3_raw, self.chan4_raw, self.chan5_raw, self.chan6_raw, self.chan7_raw, self.chan8_raw, self.chan9_raw, self.chan10_raw, self.chan11_raw, self.chan12_raw, self.rssi))

class MAVLink_optical_flow_message(MAVLink_message):
        '''
        Optical flow from a flow sensor (e.g. optical mouse sensor)
        '''
        id = MAVLINK_MSG_ID_OPTICAL_FLOW
        name = 'OPTICAL_FLOW'
        fieldnames = ['time_usec', 'sensor_id', 'flow_x', 'flow_y', 'flow_comp_m_x', 'flow_comp_m_y', 'quality', 'ground_distance']
        ordered_fieldnames = [ 'time_usec', 'flow_comp_m_x', 'flow_comp_m_y', 'ground_distance', 'flow_x', 'flow_y', 'sensor_id', 'quality' ]
        format = '<QfffhhBB'
        native_format = bytearray('<QfffhhBB', 'ascii')
        orders = [0, 6, 4, 5, 1, 2, 7, 3]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 175

        def __init__(self, time_usec, sensor_id, flow_x, flow_y, flow_comp_m_x, flow_comp_m_y, quality, ground_distance):
                MAVLink_message.__init__(self, MAVLink_optical_flow_message.id, MAVLink_optical_flow_message.name)
                self._fieldnames = MAVLink_optical_flow_message.fieldnames
                self.time_usec = time_usec
                self.sensor_id = sensor_id
                self.flow_x = flow_x
                self.flow_y = flow_y
                self.flow_comp_m_x = flow_comp_m_x
                self.flow_comp_m_y = flow_comp_m_y
                self.quality = quality
                self.ground_distance = ground_distance

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 175, struct.pack('<QfffhhBB', self.time_usec, self.flow_comp_m_x, self.flow_comp_m_y, self.ground_distance, self.flow_x, self.flow_y, self.sensor_id, self.quality))

class MAVLink_global_vision_position_estimate_message(MAVLink_message):
        '''

        '''
        id = MAVLINK_MSG_ID_GLOBAL_VISION_POSITION_ESTIMATE
        name = 'GLOBAL_VISION_POSITION_ESTIMATE'
        fieldnames = ['usec', 'x', 'y', 'z', 'roll', 'pitch', 'yaw']
        ordered_fieldnames = [ 'usec', 'x', 'y', 'z', 'roll', 'pitch', 'yaw' ]
        format = '<Qffffff'
        native_format = bytearray('<Qffffff', 'ascii')
        orders = [0, 1, 2, 3, 4, 5, 6]
        lengths = [1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0]
        crc_extra = 102

        def __init__(self, usec, x, y, z, roll, pitch, yaw):
                MAVLink_message.__init__(self, MAVLink_global_vision_position_estimate_message.id, MAVLink_global_vision_position_estimate_message.name)
                self._fieldnames = MAVLink_global_vision_position_estimate_message.fieldnames
                self.usec = usec
                self.x = x
                self.y = y
                self.z = z
                self.roll = roll
                self.pitch = pitch
                self.yaw = yaw

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 102, struct.pack('<Qffffff', self.usec, self.x, self.y, self.z, self.roll, self.pitch, self.yaw))

class MAVLink_vision_position_estimate_message(MAVLink_message):
        '''

        '''
        id = MAVLINK_MSG_ID_VISION_POSITION_ESTIMATE
        name = 'VISION_POSITION_ESTIMATE'
        fieldnames = ['usec', 'x', 'y', 'z', 'roll', 'pitch', 'yaw']
        ordered_fieldnames = [ 'usec', 'x', 'y', 'z', 'roll', 'pitch', 'yaw' ]
        format = '<Qffffff'
        native_format = bytearray('<Qffffff', 'ascii')
        orders = [0, 1, 2, 3, 4, 5, 6]
        lengths = [1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0]
        crc_extra = 158

        def __init__(self, usec, x, y, z, roll, pitch, yaw):
                MAVLink_message.__init__(self, MAVLink_vision_position_estimate_message.id, MAVLink_vision_position_estimate_message.name)
                self._fieldnames = MAVLink_vision_position_estimate_message.fieldnames
                self.usec = usec
                self.x = x
                self.y = y
                self.z = z
                self.roll = roll
                self.pitch = pitch
                self.yaw = yaw

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 158, struct.pack('<Qffffff', self.usec, self.x, self.y, self.z, self.roll, self.pitch, self.yaw))

class MAVLink_vision_speed_estimate_message(MAVLink_message):
        '''

        '''
        id = MAVLINK_MSG_ID_VISION_SPEED_ESTIMATE
        name = 'VISION_SPEED_ESTIMATE'
        fieldnames = ['usec', 'x', 'y', 'z']
        ordered_fieldnames = [ 'usec', 'x', 'y', 'z' ]
        format = '<Qfff'
        native_format = bytearray('<Qfff', 'ascii')
        orders = [0, 1, 2, 3]
        lengths = [1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0]
        crc_extra = 208

        def __init__(self, usec, x, y, z):
                MAVLink_message.__init__(self, MAVLink_vision_speed_estimate_message.id, MAVLink_vision_speed_estimate_message.name)
                self._fieldnames = MAVLink_vision_speed_estimate_message.fieldnames
                self.usec = usec
                self.x = x
                self.y = y
                self.z = z

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 208, struct.pack('<Qfff', self.usec, self.x, self.y, self.z))

class MAVLink_vicon_position_estimate_message(MAVLink_message):
        '''

        '''
        id = MAVLINK_MSG_ID_VICON_POSITION_ESTIMATE
        name = 'VICON_POSITION_ESTIMATE'
        fieldnames = ['usec', 'x', 'y', 'z', 'roll', 'pitch', 'yaw']
        ordered_fieldnames = [ 'usec', 'x', 'y', 'z', 'roll', 'pitch', 'yaw' ]
        format = '<Qffffff'
        native_format = bytearray('<Qffffff', 'ascii')
        orders = [0, 1, 2, 3, 4, 5, 6]
        lengths = [1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0]
        crc_extra = 56

        def __init__(self, usec, x, y, z, roll, pitch, yaw):
                MAVLink_message.__init__(self, MAVLink_vicon_position_estimate_message.id, MAVLink_vicon_position_estimate_message.name)
                self._fieldnames = MAVLink_vicon_position_estimate_message.fieldnames
                self.usec = usec
                self.x = x
                self.y = y
                self.z = z
                self.roll = roll
                self.pitch = pitch
                self.yaw = yaw

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 56, struct.pack('<Qffffff', self.usec, self.x, self.y, self.z, self.roll, self.pitch, self.yaw))

class MAVLink_highres_imu_message(MAVLink_message):
        '''
        The IMU readings in SI units in NED body frame
        '''
        id = MAVLINK_MSG_ID_HIGHRES_IMU
        name = 'HIGHRES_IMU'
        fieldnames = ['time_usec', 'xacc', 'yacc', 'zacc', 'xgyro', 'ygyro', 'zgyro', 'xmag', 'ymag', 'zmag', 'abs_pressure', 'diff_pressure', 'pressure_alt', 'temperature', 'fields_updated']
        ordered_fieldnames = [ 'time_usec', 'xacc', 'yacc', 'zacc', 'xgyro', 'ygyro', 'zgyro', 'xmag', 'ymag', 'zmag', 'abs_pressure', 'diff_pressure', 'pressure_alt', 'temperature', 'fields_updated' ]
        format = '<QfffffffffffffH'
        native_format = bytearray('<QfffffffffffffH', 'ascii')
        orders = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 93

        def __init__(self, time_usec, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag, abs_pressure, diff_pressure, pressure_alt, temperature, fields_updated):
                MAVLink_message.__init__(self, MAVLink_highres_imu_message.id, MAVLink_highres_imu_message.name)
                self._fieldnames = MAVLink_highres_imu_message.fieldnames
                self.time_usec = time_usec
                self.xacc = xacc
                self.yacc = yacc
                self.zacc = zacc
                self.xgyro = xgyro
                self.ygyro = ygyro
                self.zgyro = zgyro
                self.xmag = xmag
                self.ymag = ymag
                self.zmag = zmag
                self.abs_pressure = abs_pressure
                self.diff_pressure = diff_pressure
                self.pressure_alt = pressure_alt
                self.temperature = temperature
                self.fields_updated = fields_updated

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 93, struct.pack('<QfffffffffffffH', self.time_usec, self.xacc, self.yacc, self.zacc, self.xgyro, self.ygyro, self.zgyro, self.xmag, self.ymag, self.zmag, self.abs_pressure, self.diff_pressure, self.pressure_alt, self.temperature, self.fields_updated))

class MAVLink_optical_flow_rad_message(MAVLink_message):
        '''
        Optical flow from an angular rate flow sensor (e.g. PX4FLOW or
        mouse sensor)
        '''
        id = MAVLINK_MSG_ID_OPTICAL_FLOW_RAD
        name = 'OPTICAL_FLOW_RAD'
        fieldnames = ['time_usec', 'sensor_id', 'integration_time_us', 'integrated_x', 'integrated_y', 'integrated_xgyro', 'integrated_ygyro', 'integrated_zgyro', 'temperature', 'quality', 'time_delta_distance_us', 'distance']
        ordered_fieldnames = [ 'time_usec', 'integration_time_us', 'integrated_x', 'integrated_y', 'integrated_xgyro', 'integrated_ygyro', 'integrated_zgyro', 'time_delta_distance_us', 'distance', 'temperature', 'sensor_id', 'quality' ]
        format = '<QIfffffIfhBB'
        native_format = bytearray('<QIfffffIfhBB', 'ascii')
        orders = [0, 10, 1, 2, 3, 4, 5, 6, 9, 11, 7, 8]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 138

        def __init__(self, time_usec, sensor_id, integration_time_us, integrated_x, integrated_y, integrated_xgyro, integrated_ygyro, integrated_zgyro, temperature, quality, time_delta_distance_us, distance):
                MAVLink_message.__init__(self, MAVLink_optical_flow_rad_message.id, MAVLink_optical_flow_rad_message.name)
                self._fieldnames = MAVLink_optical_flow_rad_message.fieldnames
                self.time_usec = time_usec
                self.sensor_id = sensor_id
                self.integration_time_us = integration_time_us
                self.integrated_x = integrated_x
                self.integrated_y = integrated_y
                self.integrated_xgyro = integrated_xgyro
                self.integrated_ygyro = integrated_ygyro
                self.integrated_zgyro = integrated_zgyro
                self.temperature = temperature
                self.quality = quality
                self.time_delta_distance_us = time_delta_distance_us
                self.distance = distance

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 138, struct.pack('<QIfffffIfhBB', self.time_usec, self.integration_time_us, self.integrated_x, self.integrated_y, self.integrated_xgyro, self.integrated_ygyro, self.integrated_zgyro, self.time_delta_distance_us, self.distance, self.temperature, self.sensor_id, self.quality))

class MAVLink_hil_sensor_message(MAVLink_message):
        '''
        The IMU readings in SI units in NED body frame
        '''
        id = MAVLINK_MSG_ID_HIL_SENSOR
        name = 'HIL_SENSOR'
        fieldnames = ['time_usec', 'xacc', 'yacc', 'zacc', 'xgyro', 'ygyro', 'zgyro', 'xmag', 'ymag', 'zmag', 'abs_pressure', 'diff_pressure', 'pressure_alt', 'temperature', 'fields_updated']
        ordered_fieldnames = [ 'time_usec', 'xacc', 'yacc', 'zacc', 'xgyro', 'ygyro', 'zgyro', 'xmag', 'ymag', 'zmag', 'abs_pressure', 'diff_pressure', 'pressure_alt', 'temperature', 'fields_updated' ]
        format = '<QfffffffffffffI'
        native_format = bytearray('<QfffffffffffffI', 'ascii')
        orders = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 108

        def __init__(self, time_usec, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag, abs_pressure, diff_pressure, pressure_alt, temperature, fields_updated):
                MAVLink_message.__init__(self, MAVLink_hil_sensor_message.id, MAVLink_hil_sensor_message.name)
                self._fieldnames = MAVLink_hil_sensor_message.fieldnames
                self.time_usec = time_usec
                self.xacc = xacc
                self.yacc = yacc
                self.zacc = zacc
                self.xgyro = xgyro
                self.ygyro = ygyro
                self.zgyro = zgyro
                self.xmag = xmag
                self.ymag = ymag
                self.zmag = zmag
                self.abs_pressure = abs_pressure
                self.diff_pressure = diff_pressure
                self.pressure_alt = pressure_alt
                self.temperature = temperature
                self.fields_updated = fields_updated

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 108, struct.pack('<QfffffffffffffI', self.time_usec, self.xacc, self.yacc, self.zacc, self.xgyro, self.ygyro, self.zgyro, self.xmag, self.ymag, self.zmag, self.abs_pressure, self.diff_pressure, self.pressure_alt, self.temperature, self.fields_updated))

class MAVLink_sim_state_message(MAVLink_message):
        '''
        Status of simulation environment, if used
        '''
        id = MAVLINK_MSG_ID_SIM_STATE
        name = 'SIM_STATE'
        fieldnames = ['q1', 'q2', 'q3', 'q4', 'roll', 'pitch', 'yaw', 'xacc', 'yacc', 'zacc', 'xgyro', 'ygyro', 'zgyro', 'lat', 'lon', 'alt', 'std_dev_horz', 'std_dev_vert', 'vn', 've', 'vd']
        ordered_fieldnames = [ 'q1', 'q2', 'q3', 'q4', 'roll', 'pitch', 'yaw', 'xacc', 'yacc', 'zacc', 'xgyro', 'ygyro', 'zgyro', 'lat', 'lon', 'alt', 'std_dev_horz', 'std_dev_vert', 'vn', 've', 'vd' ]
        format = '<fffffffffffffffffffff'
        native_format = bytearray('<fffffffffffffffffffff', 'ascii')
        orders = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 32

        def __init__(self, q1, q2, q3, q4, roll, pitch, yaw, xacc, yacc, zacc, xgyro, ygyro, zgyro, lat, lon, alt, std_dev_horz, std_dev_vert, vn, ve, vd):
                MAVLink_message.__init__(self, MAVLink_sim_state_message.id, MAVLink_sim_state_message.name)
                self._fieldnames = MAVLink_sim_state_message.fieldnames
                self.q1 = q1
                self.q2 = q2
                self.q3 = q3
                self.q4 = q4
                self.roll = roll
                self.pitch = pitch
                self.yaw = yaw
                self.xacc = xacc
                self.yacc = yacc
                self.zacc = zacc
                self.xgyro = xgyro
                self.ygyro = ygyro
                self.zgyro = zgyro
                self.lat = lat
                self.lon = lon
                self.alt = alt
                self.std_dev_horz = std_dev_horz
                self.std_dev_vert = std_dev_vert
                self.vn = vn
                self.ve = ve
                self.vd = vd

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 32, struct.pack('<fffffffffffffffffffff', self.q1, self.q2, self.q3, self.q4, self.roll, self.pitch, self.yaw, self.xacc, self.yacc, self.zacc, self.xgyro, self.ygyro, self.zgyro, self.lat, self.lon, self.alt, self.std_dev_horz, self.std_dev_vert, self.vn, self.ve, self.vd))

class MAVLink_radio_status_message(MAVLink_message):
        '''
        Status generated by radio and injected into MAVLink stream.
        '''
        id = MAVLINK_MSG_ID_RADIO_STATUS
        name = 'RADIO_STATUS'
        fieldnames = ['rssi', 'remrssi', 'txbuf', 'noise', 'remnoise', 'rxerrors', 'fixed']
        ordered_fieldnames = [ 'rxerrors', 'fixed', 'rssi', 'remrssi', 'txbuf', 'noise', 'remnoise' ]
        format = '<HHBBBBB'
        native_format = bytearray('<HHBBBBB', 'ascii')
        orders = [2, 3, 4, 5, 6, 0, 1]
        lengths = [1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0]
        crc_extra = 185

        def __init__(self, rssi, remrssi, txbuf, noise, remnoise, rxerrors, fixed):
                MAVLink_message.__init__(self, MAVLink_radio_status_message.id, MAVLink_radio_status_message.name)
                self._fieldnames = MAVLink_radio_status_message.fieldnames
                self.rssi = rssi
                self.remrssi = remrssi
                self.txbuf = txbuf
                self.noise = noise
                self.remnoise = remnoise
                self.rxerrors = rxerrors
                self.fixed = fixed

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 185, struct.pack('<HHBBBBB', self.rxerrors, self.fixed, self.rssi, self.remrssi, self.txbuf, self.noise, self.remnoise))

class MAVLink_file_transfer_protocol_message(MAVLink_message):
        '''
        File transfer message
        '''
        id = MAVLINK_MSG_ID_FILE_TRANSFER_PROTOCOL
        name = 'FILE_TRANSFER_PROTOCOL'
        fieldnames = ['target_network', 'target_system', 'target_component', 'payload']
        ordered_fieldnames = [ 'target_network', 'target_system', 'target_component', 'payload' ]
        format = '<BBB251B'
        native_format = bytearray('<BBBB', 'ascii')
        orders = [0, 1, 2, 3]
        lengths = [1, 1, 1, 251]
        array_lengths = [0, 0, 0, 251]
        crc_extra = 84

        def __init__(self, target_network, target_system, target_component, payload):
                MAVLink_message.__init__(self, MAVLink_file_transfer_protocol_message.id, MAVLink_file_transfer_protocol_message.name)
                self._fieldnames = MAVLink_file_transfer_protocol_message.fieldnames
                self.target_network = target_network
                self.target_system = target_system
                self.target_component = target_component
                self.payload = payload

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 84, struct.pack('<BBB251B', self.target_network, self.target_system, self.target_component, self.payload[0], self.payload[1], self.payload[2], self.payload[3], self.payload[4], self.payload[5], self.payload[6], self.payload[7], self.payload[8], self.payload[9], self.payload[10], self.payload[11], self.payload[12], self.payload[13], self.payload[14], self.payload[15], self.payload[16], self.payload[17], self.payload[18], self.payload[19], self.payload[20], self.payload[21], self.payload[22], self.payload[23], self.payload[24], self.payload[25], self.payload[26], self.payload[27], self.payload[28], self.payload[29], self.payload[30], self.payload[31], self.payload[32], self.payload[33], self.payload[34], self.payload[35], self.payload[36], self.payload[37], self.payload[38], self.payload[39], self.payload[40], self.payload[41], self.payload[42], self.payload[43], self.payload[44], self.payload[45], self.payload[46], self.payload[47], self.payload[48], self.payload[49], self.payload[50], self.payload[51], self.payload[52], self.payload[53], self.payload[54], self.payload[55], self.payload[56], self.payload[57], self.payload[58], self.payload[59], self.payload[60], self.payload[61], self.payload[62], self.payload[63], self.payload[64], self.payload[65], self.payload[66], self.payload[67], self.payload[68], self.payload[69], self.payload[70], self.payload[71], self.payload[72], self.payload[73], self.payload[74], self.payload[75], self.payload[76], self.payload[77], self.payload[78], self.payload[79], self.payload[80], self.payload[81], self.payload[82], self.payload[83], self.payload[84], self.payload[85], self.payload[86], self.payload[87], self.payload[88], self.payload[89], self.payload[90], self.payload[91], self.payload[92], self.payload[93], self.payload[94], self.payload[95], self.payload[96], self.payload[97], self.payload[98], self.payload[99], self.payload[100], self.payload[101], self.payload[102], self.payload[103], self.payload[104], self.payload[105], self.payload[106], self.payload[107], self.payload[108], self.payload[109], self.payload[110], self.payload[111], self.payload[112], self.payload[113], self.payload[114], self.payload[115], self.payload[116], self.payload[117], self.payload[118], self.payload[119], self.payload[120], self.payload[121], self.payload[122], self.payload[123], self.payload[124], self.payload[125], self.payload[126], self.payload[127], self.payload[128], self.payload[129], self.payload[130], self.payload[131], self.payload[132], self.payload[133], self.payload[134], self.payload[135], self.payload[136], self.payload[137], self.payload[138], self.payload[139], self.payload[140], self.payload[141], self.payload[142], self.payload[143], self.payload[144], self.payload[145], self.payload[146], self.payload[147], self.payload[148], self.payload[149], self.payload[150], self.payload[151], self.payload[152], self.payload[153], self.payload[154], self.payload[155], self.payload[156], self.payload[157], self.payload[158], self.payload[159], self.payload[160], self.payload[161], self.payload[162], self.payload[163], self.payload[164], self.payload[165], self.payload[166], self.payload[167], self.payload[168], self.payload[169], self.payload[170], self.payload[171], self.payload[172], self.payload[173], self.payload[174], self.payload[175], self.payload[176], self.payload[177], self.payload[178], self.payload[179], self.payload[180], self.payload[181], self.payload[182], self.payload[183], self.payload[184], self.payload[185], self.payload[186], self.payload[187], self.payload[188], self.payload[189], self.payload[190], self.payload[191], self.payload[192], self.payload[193], self.payload[194], self.payload[195], self.payload[196], self.payload[197], self.payload[198], self.payload[199], self.payload[200], self.payload[201], self.payload[202], self.payload[203], self.payload[204], self.payload[205], self.payload[206], self.payload[207], self.payload[208], self.payload[209], self.payload[210], self.payload[211], self.payload[212], self.payload[213], self.payload[214], self.payload[215], self.payload[216], self.payload[217], self.payload[218], self.payload[219], self.payload[220], self.payload[221], self.payload[222], self.payload[223], self.payload[224], self.payload[225], self.payload[226], self.payload[227], self.payload[228], self.payload[229], self.payload[230], self.payload[231], self.payload[232], self.payload[233], self.payload[234], self.payload[235], self.payload[236], self.payload[237], self.payload[238], self.payload[239], self.payload[240], self.payload[241], self.payload[242], self.payload[243], self.payload[244], self.payload[245], self.payload[246], self.payload[247], self.payload[248], self.payload[249], self.payload[250]))

class MAVLink_timesync_message(MAVLink_message):
        '''
        Time synchronization message.
        '''
        id = MAVLINK_MSG_ID_TIMESYNC
        name = 'TIMESYNC'
        fieldnames = ['tc1', 'ts1']
        ordered_fieldnames = [ 'tc1', 'ts1' ]
        format = '<qq'
        native_format = bytearray('<qq', 'ascii')
        orders = [0, 1]
        lengths = [1, 1]
        array_lengths = [0, 0]
        crc_extra = 34

        def __init__(self, tc1, ts1):
                MAVLink_message.__init__(self, MAVLink_timesync_message.id, MAVLink_timesync_message.name)
                self._fieldnames = MAVLink_timesync_message.fieldnames
                self.tc1 = tc1
                self.ts1 = ts1

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 34, struct.pack('<qq', self.tc1, self.ts1))

class MAVLink_camera_trigger_message(MAVLink_message):
        '''
        Camera-IMU triggering and synchronisation message.
        '''
        id = MAVLINK_MSG_ID_CAMERA_TRIGGER
        name = 'CAMERA_TRIGGER'
        fieldnames = ['time_usec', 'seq']
        ordered_fieldnames = [ 'time_usec', 'seq' ]
        format = '<QI'
        native_format = bytearray('<QI', 'ascii')
        orders = [0, 1]
        lengths = [1, 1]
        array_lengths = [0, 0]
        crc_extra = 174

        def __init__(self, time_usec, seq):
                MAVLink_message.__init__(self, MAVLink_camera_trigger_message.id, MAVLink_camera_trigger_message.name)
                self._fieldnames = MAVLink_camera_trigger_message.fieldnames
                self.time_usec = time_usec
                self.seq = seq

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 174, struct.pack('<QI', self.time_usec, self.seq))

class MAVLink_hil_gps_message(MAVLink_message):
        '''
        The global position, as returned by the Global Positioning
        System (GPS). This is                  NOT the global position
        estimate of the sytem, but rather a RAW sensor value. See
        message GLOBAL_POSITION for the global position estimate.
        Coordinate frame is right-handed, Z-axis up (GPS frame).
        '''
        id = MAVLINK_MSG_ID_HIL_GPS
        name = 'HIL_GPS'
        fieldnames = ['time_usec', 'fix_type', 'lat', 'lon', 'alt', 'eph', 'epv', 'vel', 'vn', 've', 'vd', 'cog', 'satellites_visible']
        ordered_fieldnames = [ 'time_usec', 'lat', 'lon', 'alt', 'eph', 'epv', 'vel', 'vn', 've', 'vd', 'cog', 'fix_type', 'satellites_visible' ]
        format = '<QiiiHHHhhhHBB'
        native_format = bytearray('<QiiiHHHhhhHBB', 'ascii')
        orders = [0, 11, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 12]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 124

        def __init__(self, time_usec, fix_type, lat, lon, alt, eph, epv, vel, vn, ve, vd, cog, satellites_visible):
                MAVLink_message.__init__(self, MAVLink_hil_gps_message.id, MAVLink_hil_gps_message.name)
                self._fieldnames = MAVLink_hil_gps_message.fieldnames
                self.time_usec = time_usec
                self.fix_type = fix_type
                self.lat = lat
                self.lon = lon
                self.alt = alt
                self.eph = eph
                self.epv = epv
                self.vel = vel
                self.vn = vn
                self.ve = ve
                self.vd = vd
                self.cog = cog
                self.satellites_visible = satellites_visible

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 124, struct.pack('<QiiiHHHhhhHBB', self.time_usec, self.lat, self.lon, self.alt, self.eph, self.epv, self.vel, self.vn, self.ve, self.vd, self.cog, self.fix_type, self.satellites_visible))

class MAVLink_hil_optical_flow_message(MAVLink_message):
        '''
        Simulated optical flow from a flow sensor (e.g. PX4FLOW or
        optical mouse sensor)
        '''
        id = MAVLINK_MSG_ID_HIL_OPTICAL_FLOW
        name = 'HIL_OPTICAL_FLOW'
        fieldnames = ['time_usec', 'sensor_id', 'integration_time_us', 'integrated_x', 'integrated_y', 'integrated_xgyro', 'integrated_ygyro', 'integrated_zgyro', 'temperature', 'quality', 'time_delta_distance_us', 'distance']
        ordered_fieldnames = [ 'time_usec', 'integration_time_us', 'integrated_x', 'integrated_y', 'integrated_xgyro', 'integrated_ygyro', 'integrated_zgyro', 'time_delta_distance_us', 'distance', 'temperature', 'sensor_id', 'quality' ]
        format = '<QIfffffIfhBB'
        native_format = bytearray('<QIfffffIfhBB', 'ascii')
        orders = [0, 10, 1, 2, 3, 4, 5, 6, 9, 11, 7, 8]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 237

        def __init__(self, time_usec, sensor_id, integration_time_us, integrated_x, integrated_y, integrated_xgyro, integrated_ygyro, integrated_zgyro, temperature, quality, time_delta_distance_us, distance):
                MAVLink_message.__init__(self, MAVLink_hil_optical_flow_message.id, MAVLink_hil_optical_flow_message.name)
                self._fieldnames = MAVLink_hil_optical_flow_message.fieldnames
                self.time_usec = time_usec
                self.sensor_id = sensor_id
                self.integration_time_us = integration_time_us
                self.integrated_x = integrated_x
                self.integrated_y = integrated_y
                self.integrated_xgyro = integrated_xgyro
                self.integrated_ygyro = integrated_ygyro
                self.integrated_zgyro = integrated_zgyro
                self.temperature = temperature
                self.quality = quality
                self.time_delta_distance_us = time_delta_distance_us
                self.distance = distance

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 237, struct.pack('<QIfffffIfhBB', self.time_usec, self.integration_time_us, self.integrated_x, self.integrated_y, self.integrated_xgyro, self.integrated_ygyro, self.integrated_zgyro, self.time_delta_distance_us, self.distance, self.temperature, self.sensor_id, self.quality))

class MAVLink_hil_state_quaternion_message(MAVLink_message):
        '''
        Sent from simulation to autopilot, avoids in contrast to
        HIL_STATE singularities. This packet is useful for high
        throughput applications such as hardware in the loop
        simulations.
        '''
        id = MAVLINK_MSG_ID_HIL_STATE_QUATERNION
        name = 'HIL_STATE_QUATERNION'
        fieldnames = ['time_usec', 'attitude_quaternion', 'rollspeed', 'pitchspeed', 'yawspeed', 'lat', 'lon', 'alt', 'vx', 'vy', 'vz', 'ind_airspeed', 'true_airspeed', 'xacc', 'yacc', 'zacc']
        ordered_fieldnames = [ 'time_usec', 'attitude_quaternion', 'rollspeed', 'pitchspeed', 'yawspeed', 'lat', 'lon', 'alt', 'vx', 'vy', 'vz', 'ind_airspeed', 'true_airspeed', 'xacc', 'yacc', 'zacc' ]
        format = '<Q4ffffiiihhhHHhhh'
        native_format = bytearray('<QffffiiihhhHHhhh', 'ascii')
        orders = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15]
        lengths = [1, 4, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 4, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 4

        def __init__(self, time_usec, attitude_quaternion, rollspeed, pitchspeed, yawspeed, lat, lon, alt, vx, vy, vz, ind_airspeed, true_airspeed, xacc, yacc, zacc):
                MAVLink_message.__init__(self, MAVLink_hil_state_quaternion_message.id, MAVLink_hil_state_quaternion_message.name)
                self._fieldnames = MAVLink_hil_state_quaternion_message.fieldnames
                self.time_usec = time_usec
                self.attitude_quaternion = attitude_quaternion
                self.rollspeed = rollspeed
                self.pitchspeed = pitchspeed
                self.yawspeed = yawspeed
                self.lat = lat
                self.lon = lon
                self.alt = alt
                self.vx = vx
                self.vy = vy
                self.vz = vz
                self.ind_airspeed = ind_airspeed
                self.true_airspeed = true_airspeed
                self.xacc = xacc
                self.yacc = yacc
                self.zacc = zacc

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 4, struct.pack('<Q4ffffiiihhhHHhhh', self.time_usec, self.attitude_quaternion[0], self.attitude_quaternion[1], self.attitude_quaternion[2], self.attitude_quaternion[3], self.rollspeed, self.pitchspeed, self.yawspeed, self.lat, self.lon, self.alt, self.vx, self.vy, self.vz, self.ind_airspeed, self.true_airspeed, self.xacc, self.yacc, self.zacc))

class MAVLink_scaled_imu2_message(MAVLink_message):
        '''
        The RAW IMU readings for secondary 9DOF sensor setup. This
        message should contain the scaled values to the described
        units
        '''
        id = MAVLINK_MSG_ID_SCALED_IMU2
        name = 'SCALED_IMU2'
        fieldnames = ['time_boot_ms', 'xacc', 'yacc', 'zacc', 'xgyro', 'ygyro', 'zgyro', 'xmag', 'ymag', 'zmag']
        ordered_fieldnames = [ 'time_boot_ms', 'xacc', 'yacc', 'zacc', 'xgyro', 'ygyro', 'zgyro', 'xmag', 'ymag', 'zmag' ]
        format = '<Ihhhhhhhhh'
        native_format = bytearray('<Ihhhhhhhhh', 'ascii')
        orders = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 76

        def __init__(self, time_boot_ms, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag):
                MAVLink_message.__init__(self, MAVLink_scaled_imu2_message.id, MAVLink_scaled_imu2_message.name)
                self._fieldnames = MAVLink_scaled_imu2_message.fieldnames
                self.time_boot_ms = time_boot_ms
                self.xacc = xacc
                self.yacc = yacc
                self.zacc = zacc
                self.xgyro = xgyro
                self.ygyro = ygyro
                self.zgyro = zgyro
                self.xmag = xmag
                self.ymag = ymag
                self.zmag = zmag

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 76, struct.pack('<Ihhhhhhhhh', self.time_boot_ms, self.xacc, self.yacc, self.zacc, self.xgyro, self.ygyro, self.zgyro, self.xmag, self.ymag, self.zmag))

class MAVLink_log_request_list_message(MAVLink_message):
        '''
        Request a list of available logs. On some systems calling this
        may stop on-board logging until LOG_REQUEST_END is called.
        '''
        id = MAVLINK_MSG_ID_LOG_REQUEST_LIST
        name = 'LOG_REQUEST_LIST'
        fieldnames = ['target_system', 'target_component', 'start', 'end']
        ordered_fieldnames = [ 'start', 'end', 'target_system', 'target_component' ]
        format = '<HHBB'
        native_format = bytearray('<HHBB', 'ascii')
        orders = [2, 3, 0, 1]
        lengths = [1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0]
        crc_extra = 128

        def __init__(self, target_system, target_component, start, end):
                MAVLink_message.__init__(self, MAVLink_log_request_list_message.id, MAVLink_log_request_list_message.name)
                self._fieldnames = MAVLink_log_request_list_message.fieldnames
                self.target_system = target_system
                self.target_component = target_component
                self.start = start
                self.end = end

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 128, struct.pack('<HHBB', self.start, self.end, self.target_system, self.target_component))

class MAVLink_log_entry_message(MAVLink_message):
        '''
        Reply to LOG_REQUEST_LIST
        '''
        id = MAVLINK_MSG_ID_LOG_ENTRY
        name = 'LOG_ENTRY'
        fieldnames = ['id', 'num_logs', 'last_log_num', 'time_utc', 'size']
        ordered_fieldnames = [ 'time_utc', 'size', 'id', 'num_logs', 'last_log_num' ]
        format = '<IIHHH'
        native_format = bytearray('<IIHHH', 'ascii')
        orders = [2, 3, 4, 0, 1]
        lengths = [1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0]
        crc_extra = 56

        def __init__(self, id, num_logs, last_log_num, time_utc, size):
                MAVLink_message.__init__(self, MAVLink_log_entry_message.id, MAVLink_log_entry_message.name)
                self._fieldnames = MAVLink_log_entry_message.fieldnames
                self.id = id
                self.num_logs = num_logs
                self.last_log_num = last_log_num
                self.time_utc = time_utc
                self.size = size

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 56, struct.pack('<IIHHH', self.time_utc, self.size, self.id, self.num_logs, self.last_log_num))

class MAVLink_log_request_data_message(MAVLink_message):
        '''
        Request a chunk of a log
        '''
        id = MAVLINK_MSG_ID_LOG_REQUEST_DATA
        name = 'LOG_REQUEST_DATA'
        fieldnames = ['target_system', 'target_component', 'id', 'ofs', 'count']
        ordered_fieldnames = [ 'ofs', 'count', 'id', 'target_system', 'target_component' ]
        format = '<IIHBB'
        native_format = bytearray('<IIHBB', 'ascii')
        orders = [3, 4, 2, 0, 1]
        lengths = [1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0]
        crc_extra = 116

        def __init__(self, target_system, target_component, id, ofs, count):
                MAVLink_message.__init__(self, MAVLink_log_request_data_message.id, MAVLink_log_request_data_message.name)
                self._fieldnames = MAVLink_log_request_data_message.fieldnames
                self.target_system = target_system
                self.target_component = target_component
                self.id = id
                self.ofs = ofs
                self.count = count

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 116, struct.pack('<IIHBB', self.ofs, self.count, self.id, self.target_system, self.target_component))

class MAVLink_log_data_message(MAVLink_message):
        '''
        Reply to LOG_REQUEST_DATA
        '''
        id = MAVLINK_MSG_ID_LOG_DATA
        name = 'LOG_DATA'
        fieldnames = ['id', 'ofs', 'count', 'data']
        ordered_fieldnames = [ 'ofs', 'id', 'count', 'data' ]
        format = '<IHB90B'
        native_format = bytearray('<IHBB', 'ascii')
        orders = [1, 0, 2, 3]
        lengths = [1, 1, 1, 90]
        array_lengths = [0, 0, 0, 90]
        crc_extra = 134

        def __init__(self, id, ofs, count, data):
                MAVLink_message.__init__(self, MAVLink_log_data_message.id, MAVLink_log_data_message.name)
                self._fieldnames = MAVLink_log_data_message.fieldnames
                self.id = id
                self.ofs = ofs
                self.count = count
                self.data = data

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 134, struct.pack('<IHB90B', self.ofs, self.id, self.count, self.data[0], self.data[1], self.data[2], self.data[3], self.data[4], self.data[5], self.data[6], self.data[7], self.data[8], self.data[9], self.data[10], self.data[11], self.data[12], self.data[13], self.data[14], self.data[15], self.data[16], self.data[17], self.data[18], self.data[19], self.data[20], self.data[21], self.data[22], self.data[23], self.data[24], self.data[25], self.data[26], self.data[27], self.data[28], self.data[29], self.data[30], self.data[31], self.data[32], self.data[33], self.data[34], self.data[35], self.data[36], self.data[37], self.data[38], self.data[39], self.data[40], self.data[41], self.data[42], self.data[43], self.data[44], self.data[45], self.data[46], self.data[47], self.data[48], self.data[49], self.data[50], self.data[51], self.data[52], self.data[53], self.data[54], self.data[55], self.data[56], self.data[57], self.data[58], self.data[59], self.data[60], self.data[61], self.data[62], self.data[63], self.data[64], self.data[65], self.data[66], self.data[67], self.data[68], self.data[69], self.data[70], self.data[71], self.data[72], self.data[73], self.data[74], self.data[75], self.data[76], self.data[77], self.data[78], self.data[79], self.data[80], self.data[81], self.data[82], self.data[83], self.data[84], self.data[85], self.data[86], self.data[87], self.data[88], self.data[89]))

class MAVLink_log_erase_message(MAVLink_message):
        '''
        Erase all logs
        '''
        id = MAVLINK_MSG_ID_LOG_ERASE
        name = 'LOG_ERASE'
        fieldnames = ['target_system', 'target_component']
        ordered_fieldnames = [ 'target_system', 'target_component' ]
        format = '<BB'
        native_format = bytearray('<BB', 'ascii')
        orders = [0, 1]
        lengths = [1, 1]
        array_lengths = [0, 0]
        crc_extra = 237

        def __init__(self, target_system, target_component):
                MAVLink_message.__init__(self, MAVLink_log_erase_message.id, MAVLink_log_erase_message.name)
                self._fieldnames = MAVLink_log_erase_message.fieldnames
                self.target_system = target_system
                self.target_component = target_component

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 237, struct.pack('<BB', self.target_system, self.target_component))

class MAVLink_log_request_end_message(MAVLink_message):
        '''
        Stop log transfer and resume normal logging
        '''
        id = MAVLINK_MSG_ID_LOG_REQUEST_END
        name = 'LOG_REQUEST_END'
        fieldnames = ['target_system', 'target_component']
        ordered_fieldnames = [ 'target_system', 'target_component' ]
        format = '<BB'
        native_format = bytearray('<BB', 'ascii')
        orders = [0, 1]
        lengths = [1, 1]
        array_lengths = [0, 0]
        crc_extra = 203

        def __init__(self, target_system, target_component):
                MAVLink_message.__init__(self, MAVLink_log_request_end_message.id, MAVLink_log_request_end_message.name)
                self._fieldnames = MAVLink_log_request_end_message.fieldnames
                self.target_system = target_system
                self.target_component = target_component

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 203, struct.pack('<BB', self.target_system, self.target_component))

class MAVLink_gps_inject_data_message(MAVLink_message):
        '''
        data for injecting into the onboard GPS (used for DGPS)
        '''
        id = MAVLINK_MSG_ID_GPS_INJECT_DATA
        name = 'GPS_INJECT_DATA'
        fieldnames = ['target_system', 'target_component', 'len', 'data']
        ordered_fieldnames = [ 'target_system', 'target_component', 'len', 'data' ]
        format = '<BBB110B'
        native_format = bytearray('<BBBB', 'ascii')
        orders = [0, 1, 2, 3]
        lengths = [1, 1, 1, 110]
        array_lengths = [0, 0, 0, 110]
        crc_extra = 250

        def __init__(self, target_system, target_component, len, data):
                MAVLink_message.__init__(self, MAVLink_gps_inject_data_message.id, MAVLink_gps_inject_data_message.name)
                self._fieldnames = MAVLink_gps_inject_data_message.fieldnames
                self.target_system = target_system
                self.target_component = target_component
                self.len = len
                self.data = data

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 250, struct.pack('<BBB110B', self.target_system, self.target_component, self.len, self.data[0], self.data[1], self.data[2], self.data[3], self.data[4], self.data[5], self.data[6], self.data[7], self.data[8], self.data[9], self.data[10], self.data[11], self.data[12], self.data[13], self.data[14], self.data[15], self.data[16], self.data[17], self.data[18], self.data[19], self.data[20], self.data[21], self.data[22], self.data[23], self.data[24], self.data[25], self.data[26], self.data[27], self.data[28], self.data[29], self.data[30], self.data[31], self.data[32], self.data[33], self.data[34], self.data[35], self.data[36], self.data[37], self.data[38], self.data[39], self.data[40], self.data[41], self.data[42], self.data[43], self.data[44], self.data[45], self.data[46], self.data[47], self.data[48], self.data[49], self.data[50], self.data[51], self.data[52], self.data[53], self.data[54], self.data[55], self.data[56], self.data[57], self.data[58], self.data[59], self.data[60], self.data[61], self.data[62], self.data[63], self.data[64], self.data[65], self.data[66], self.data[67], self.data[68], self.data[69], self.data[70], self.data[71], self.data[72], self.data[73], self.data[74], self.data[75], self.data[76], self.data[77], self.data[78], self.data[79], self.data[80], self.data[81], self.data[82], self.data[83], self.data[84], self.data[85], self.data[86], self.data[87], self.data[88], self.data[89], self.data[90], self.data[91], self.data[92], self.data[93], self.data[94], self.data[95], self.data[96], self.data[97], self.data[98], self.data[99], self.data[100], self.data[101], self.data[102], self.data[103], self.data[104], self.data[105], self.data[106], self.data[107], self.data[108], self.data[109]))

class MAVLink_gps2_raw_message(MAVLink_message):
        '''
        Second GPS data. Coordinate frame is right-handed, Z-axis up
        (GPS frame).
        '''
        id = MAVLINK_MSG_ID_GPS2_RAW
        name = 'GPS2_RAW'
        fieldnames = ['time_usec', 'fix_type', 'lat', 'lon', 'alt', 'eph', 'epv', 'vel', 'cog', 'satellites_visible', 'dgps_numch', 'dgps_age']
        ordered_fieldnames = [ 'time_usec', 'lat', 'lon', 'alt', 'dgps_age', 'eph', 'epv', 'vel', 'cog', 'fix_type', 'satellites_visible', 'dgps_numch' ]
        format = '<QiiiIHHHHBBB'
        native_format = bytearray('<QiiiIHHHHBBB', 'ascii')
        orders = [0, 9, 1, 2, 3, 5, 6, 7, 8, 10, 11, 4]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 87

        def __init__(self, time_usec, fix_type, lat, lon, alt, eph, epv, vel, cog, satellites_visible, dgps_numch, dgps_age):
                MAVLink_message.__init__(self, MAVLink_gps2_raw_message.id, MAVLink_gps2_raw_message.name)
                self._fieldnames = MAVLink_gps2_raw_message.fieldnames
                self.time_usec = time_usec
                self.fix_type = fix_type
                self.lat = lat
                self.lon = lon
                self.alt = alt
                self.eph = eph
                self.epv = epv
                self.vel = vel
                self.cog = cog
                self.satellites_visible = satellites_visible
                self.dgps_numch = dgps_numch
                self.dgps_age = dgps_age

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 87, struct.pack('<QiiiIHHHHBBB', self.time_usec, self.lat, self.lon, self.alt, self.dgps_age, self.eph, self.epv, self.vel, self.cog, self.fix_type, self.satellites_visible, self.dgps_numch))

class MAVLink_power_status_message(MAVLink_message):
        '''
        Power supply status
        '''
        id = MAVLINK_MSG_ID_POWER_STATUS
        name = 'POWER_STATUS'
        fieldnames = ['Vcc', 'Vservo', 'flags']
        ordered_fieldnames = [ 'Vcc', 'Vservo', 'flags' ]
        format = '<HHH'
        native_format = bytearray('<HHH', 'ascii')
        orders = [0, 1, 2]
        lengths = [1, 1, 1]
        array_lengths = [0, 0, 0]
        crc_extra = 203

        def __init__(self, Vcc, Vservo, flags):
                MAVLink_message.__init__(self, MAVLink_power_status_message.id, MAVLink_power_status_message.name)
                self._fieldnames = MAVLink_power_status_message.fieldnames
                self.Vcc = Vcc
                self.Vservo = Vservo
                self.flags = flags

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 203, struct.pack('<HHH', self.Vcc, self.Vservo, self.flags))

class MAVLink_serial_control_message(MAVLink_message):
        '''
        Control a serial port. This can be used for raw access to an
        onboard serial peripheral such as a GPS or telemetry radio. It
        is designed to make it possible to update the devices firmware
        via MAVLink messages or change the devices settings. A message
        with zero bytes can be used to change just the baudrate.
        '''
        id = MAVLINK_MSG_ID_SERIAL_CONTROL
        name = 'SERIAL_CONTROL'
        fieldnames = ['device', 'flags', 'timeout', 'baudrate', 'count', 'data']
        ordered_fieldnames = [ 'baudrate', 'timeout', 'device', 'flags', 'count', 'data' ]
        format = '<IHBBB70B'
        native_format = bytearray('<IHBBBB', 'ascii')
        orders = [2, 3, 1, 0, 4, 5]
        lengths = [1, 1, 1, 1, 1, 70]
        array_lengths = [0, 0, 0, 0, 0, 70]
        crc_extra = 220

        def __init__(self, device, flags, timeout, baudrate, count, data):
                MAVLink_message.__init__(self, MAVLink_serial_control_message.id, MAVLink_serial_control_message.name)
                self._fieldnames = MAVLink_serial_control_message.fieldnames
                self.device = device
                self.flags = flags
                self.timeout = timeout
                self.baudrate = baudrate
                self.count = count
                self.data = data

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 220, struct.pack('<IHBBB70B', self.baudrate, self.timeout, self.device, self.flags, self.count, self.data[0], self.data[1], self.data[2], self.data[3], self.data[4], self.data[5], self.data[6], self.data[7], self.data[8], self.data[9], self.data[10], self.data[11], self.data[12], self.data[13], self.data[14], self.data[15], self.data[16], self.data[17], self.data[18], self.data[19], self.data[20], self.data[21], self.data[22], self.data[23], self.data[24], self.data[25], self.data[26], self.data[27], self.data[28], self.data[29], self.data[30], self.data[31], self.data[32], self.data[33], self.data[34], self.data[35], self.data[36], self.data[37], self.data[38], self.data[39], self.data[40], self.data[41], self.data[42], self.data[43], self.data[44], self.data[45], self.data[46], self.data[47], self.data[48], self.data[49], self.data[50], self.data[51], self.data[52], self.data[53], self.data[54], self.data[55], self.data[56], self.data[57], self.data[58], self.data[59], self.data[60], self.data[61], self.data[62], self.data[63], self.data[64], self.data[65], self.data[66], self.data[67], self.data[68], self.data[69]))

class MAVLink_gps_rtk_message(MAVLink_message):
        '''
        RTK GPS data. Gives information on the relative baseline
        calculation the GPS is reporting
        '''
        id = MAVLINK_MSG_ID_GPS_RTK
        name = 'GPS_RTK'
        fieldnames = ['time_last_baseline_ms', 'rtk_receiver_id', 'wn', 'tow', 'rtk_health', 'rtk_rate', 'nsats', 'baseline_coords_type', 'baseline_a_mm', 'baseline_b_mm', 'baseline_c_mm', 'accuracy', 'iar_num_hypotheses']
        ordered_fieldnames = [ 'time_last_baseline_ms', 'tow', 'baseline_a_mm', 'baseline_b_mm', 'baseline_c_mm', 'accuracy', 'iar_num_hypotheses', 'wn', 'rtk_receiver_id', 'rtk_health', 'rtk_rate', 'nsats', 'baseline_coords_type' ]
        format = '<IIiiiIiHBBBBB'
        native_format = bytearray('<IIiiiIiHBBBBB', 'ascii')
        orders = [0, 8, 7, 1, 9, 10, 11, 12, 2, 3, 4, 5, 6]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 25

        def __init__(self, time_last_baseline_ms, rtk_receiver_id, wn, tow, rtk_health, rtk_rate, nsats, baseline_coords_type, baseline_a_mm, baseline_b_mm, baseline_c_mm, accuracy, iar_num_hypotheses):
                MAVLink_message.__init__(self, MAVLink_gps_rtk_message.id, MAVLink_gps_rtk_message.name)
                self._fieldnames = MAVLink_gps_rtk_message.fieldnames
                self.time_last_baseline_ms = time_last_baseline_ms
                self.rtk_receiver_id = rtk_receiver_id
                self.wn = wn
                self.tow = tow
                self.rtk_health = rtk_health
                self.rtk_rate = rtk_rate
                self.nsats = nsats
                self.baseline_coords_type = baseline_coords_type
                self.baseline_a_mm = baseline_a_mm
                self.baseline_b_mm = baseline_b_mm
                self.baseline_c_mm = baseline_c_mm
                self.accuracy = accuracy
                self.iar_num_hypotheses = iar_num_hypotheses

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 25, struct.pack('<IIiiiIiHBBBBB', self.time_last_baseline_ms, self.tow, self.baseline_a_mm, self.baseline_b_mm, self.baseline_c_mm, self.accuracy, self.iar_num_hypotheses, self.wn, self.rtk_receiver_id, self.rtk_health, self.rtk_rate, self.nsats, self.baseline_coords_type))

class MAVLink_gps2_rtk_message(MAVLink_message):
        '''
        RTK GPS data. Gives information on the relative baseline
        calculation the GPS is reporting
        '''
        id = MAVLINK_MSG_ID_GPS2_RTK
        name = 'GPS2_RTK'
        fieldnames = ['time_last_baseline_ms', 'rtk_receiver_id', 'wn', 'tow', 'rtk_health', 'rtk_rate', 'nsats', 'baseline_coords_type', 'baseline_a_mm', 'baseline_b_mm', 'baseline_c_mm', 'accuracy', 'iar_num_hypotheses']
        ordered_fieldnames = [ 'time_last_baseline_ms', 'tow', 'baseline_a_mm', 'baseline_b_mm', 'baseline_c_mm', 'accuracy', 'iar_num_hypotheses', 'wn', 'rtk_receiver_id', 'rtk_health', 'rtk_rate', 'nsats', 'baseline_coords_type' ]
        format = '<IIiiiIiHBBBBB'
        native_format = bytearray('<IIiiiIiHBBBBB', 'ascii')
        orders = [0, 8, 7, 1, 9, 10, 11, 12, 2, 3, 4, 5, 6]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 226

        def __init__(self, time_last_baseline_ms, rtk_receiver_id, wn, tow, rtk_health, rtk_rate, nsats, baseline_coords_type, baseline_a_mm, baseline_b_mm, baseline_c_mm, accuracy, iar_num_hypotheses):
                MAVLink_message.__init__(self, MAVLink_gps2_rtk_message.id, MAVLink_gps2_rtk_message.name)
                self._fieldnames = MAVLink_gps2_rtk_message.fieldnames
                self.time_last_baseline_ms = time_last_baseline_ms
                self.rtk_receiver_id = rtk_receiver_id
                self.wn = wn
                self.tow = tow
                self.rtk_health = rtk_health
                self.rtk_rate = rtk_rate
                self.nsats = nsats
                self.baseline_coords_type = baseline_coords_type
                self.baseline_a_mm = baseline_a_mm
                self.baseline_b_mm = baseline_b_mm
                self.baseline_c_mm = baseline_c_mm
                self.accuracy = accuracy
                self.iar_num_hypotheses = iar_num_hypotheses

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 226, struct.pack('<IIiiiIiHBBBBB', self.time_last_baseline_ms, self.tow, self.baseline_a_mm, self.baseline_b_mm, self.baseline_c_mm, self.accuracy, self.iar_num_hypotheses, self.wn, self.rtk_receiver_id, self.rtk_health, self.rtk_rate, self.nsats, self.baseline_coords_type))

class MAVLink_scaled_imu3_message(MAVLink_message):
        '''
        The RAW IMU readings for 3rd 9DOF sensor setup. This message
        should contain the scaled values to the described units
        '''
        id = MAVLINK_MSG_ID_SCALED_IMU3
        name = 'SCALED_IMU3'
        fieldnames = ['time_boot_ms', 'xacc', 'yacc', 'zacc', 'xgyro', 'ygyro', 'zgyro', 'xmag', 'ymag', 'zmag']
        ordered_fieldnames = [ 'time_boot_ms', 'xacc', 'yacc', 'zacc', 'xgyro', 'ygyro', 'zgyro', 'xmag', 'ymag', 'zmag' ]
        format = '<Ihhhhhhhhh'
        native_format = bytearray('<Ihhhhhhhhh', 'ascii')
        orders = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 46

        def __init__(self, time_boot_ms, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag):
                MAVLink_message.__init__(self, MAVLink_scaled_imu3_message.id, MAVLink_scaled_imu3_message.name)
                self._fieldnames = MAVLink_scaled_imu3_message.fieldnames
                self.time_boot_ms = time_boot_ms
                self.xacc = xacc
                self.yacc = yacc
                self.zacc = zacc
                self.xgyro = xgyro
                self.ygyro = ygyro
                self.zgyro = zgyro
                self.xmag = xmag
                self.ymag = ymag
                self.zmag = zmag

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 46, struct.pack('<Ihhhhhhhhh', self.time_boot_ms, self.xacc, self.yacc, self.zacc, self.xgyro, self.ygyro, self.zgyro, self.xmag, self.ymag, self.zmag))

class MAVLink_data_transmission_handshake_message(MAVLink_message):
        '''

        '''
        id = MAVLINK_MSG_ID_DATA_TRANSMISSION_HANDSHAKE
        name = 'DATA_TRANSMISSION_HANDSHAKE'
        fieldnames = ['type', 'size', 'width', 'height', 'packets', 'payload', 'jpg_quality']
        ordered_fieldnames = [ 'size', 'width', 'height', 'packets', 'type', 'payload', 'jpg_quality' ]
        format = '<IHHHBBB'
        native_format = bytearray('<IHHHBBB', 'ascii')
        orders = [4, 0, 1, 2, 3, 5, 6]
        lengths = [1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0]
        crc_extra = 29

        def __init__(self, type, size, width, height, packets, payload, jpg_quality):
                MAVLink_message.__init__(self, MAVLink_data_transmission_handshake_message.id, MAVLink_data_transmission_handshake_message.name)
                self._fieldnames = MAVLink_data_transmission_handshake_message.fieldnames
                self.type = type
                self.size = size
                self.width = width
                self.height = height
                self.packets = packets
                self.payload = payload
                self.jpg_quality = jpg_quality

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 29, struct.pack('<IHHHBBB', self.size, self.width, self.height, self.packets, self.type, self.payload, self.jpg_quality))

class MAVLink_encapsulated_data_message(MAVLink_message):
        '''

        '''
        id = MAVLINK_MSG_ID_ENCAPSULATED_DATA
        name = 'ENCAPSULATED_DATA'
        fieldnames = ['seqnr', 'data']
        ordered_fieldnames = [ 'seqnr', 'data' ]
        format = '<H253B'
        native_format = bytearray('<HB', 'ascii')
        orders = [0, 1]
        lengths = [1, 253]
        array_lengths = [0, 253]
        crc_extra = 223

        def __init__(self, seqnr, data):
                MAVLink_message.__init__(self, MAVLink_encapsulated_data_message.id, MAVLink_encapsulated_data_message.name)
                self._fieldnames = MAVLink_encapsulated_data_message.fieldnames
                self.seqnr = seqnr
                self.data = data

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 223, struct.pack('<H253B', self.seqnr, self.data[0], self.data[1], self.data[2], self.data[3], self.data[4], self.data[5], self.data[6], self.data[7], self.data[8], self.data[9], self.data[10], self.data[11], self.data[12], self.data[13], self.data[14], self.data[15], self.data[16], self.data[17], self.data[18], self.data[19], self.data[20], self.data[21], self.data[22], self.data[23], self.data[24], self.data[25], self.data[26], self.data[27], self.data[28], self.data[29], self.data[30], self.data[31], self.data[32], self.data[33], self.data[34], self.data[35], self.data[36], self.data[37], self.data[38], self.data[39], self.data[40], self.data[41], self.data[42], self.data[43], self.data[44], self.data[45], self.data[46], self.data[47], self.data[48], self.data[49], self.data[50], self.data[51], self.data[52], self.data[53], self.data[54], self.data[55], self.data[56], self.data[57], self.data[58], self.data[59], self.data[60], self.data[61], self.data[62], self.data[63], self.data[64], self.data[65], self.data[66], self.data[67], self.data[68], self.data[69], self.data[70], self.data[71], self.data[72], self.data[73], self.data[74], self.data[75], self.data[76], self.data[77], self.data[78], self.data[79], self.data[80], self.data[81], self.data[82], self.data[83], self.data[84], self.data[85], self.data[86], self.data[87], self.data[88], self.data[89], self.data[90], self.data[91], self.data[92], self.data[93], self.data[94], self.data[95], self.data[96], self.data[97], self.data[98], self.data[99], self.data[100], self.data[101], self.data[102], self.data[103], self.data[104], self.data[105], self.data[106], self.data[107], self.data[108], self.data[109], self.data[110], self.data[111], self.data[112], self.data[113], self.data[114], self.data[115], self.data[116], self.data[117], self.data[118], self.data[119], self.data[120], self.data[121], self.data[122], self.data[123], self.data[124], self.data[125], self.data[126], self.data[127], self.data[128], self.data[129], self.data[130], self.data[131], self.data[132], self.data[133], self.data[134], self.data[135], self.data[136], self.data[137], self.data[138], self.data[139], self.data[140], self.data[141], self.data[142], self.data[143], self.data[144], self.data[145], self.data[146], self.data[147], self.data[148], self.data[149], self.data[150], self.data[151], self.data[152], self.data[153], self.data[154], self.data[155], self.data[156], self.data[157], self.data[158], self.data[159], self.data[160], self.data[161], self.data[162], self.data[163], self.data[164], self.data[165], self.data[166], self.data[167], self.data[168], self.data[169], self.data[170], self.data[171], self.data[172], self.data[173], self.data[174], self.data[175], self.data[176], self.data[177], self.data[178], self.data[179], self.data[180], self.data[181], self.data[182], self.data[183], self.data[184], self.data[185], self.data[186], self.data[187], self.data[188], self.data[189], self.data[190], self.data[191], self.data[192], self.data[193], self.data[194], self.data[195], self.data[196], self.data[197], self.data[198], self.data[199], self.data[200], self.data[201], self.data[202], self.data[203], self.data[204], self.data[205], self.data[206], self.data[207], self.data[208], self.data[209], self.data[210], self.data[211], self.data[212], self.data[213], self.data[214], self.data[215], self.data[216], self.data[217], self.data[218], self.data[219], self.data[220], self.data[221], self.data[222], self.data[223], self.data[224], self.data[225], self.data[226], self.data[227], self.data[228], self.data[229], self.data[230], self.data[231], self.data[232], self.data[233], self.data[234], self.data[235], self.data[236], self.data[237], self.data[238], self.data[239], self.data[240], self.data[241], self.data[242], self.data[243], self.data[244], self.data[245], self.data[246], self.data[247], self.data[248], self.data[249], self.data[250], self.data[251], self.data[252]))

class MAVLink_distance_sensor_message(MAVLink_message):
        '''

        '''
        id = MAVLINK_MSG_ID_DISTANCE_SENSOR
        name = 'DISTANCE_SENSOR'
        fieldnames = ['time_boot_ms', 'min_distance', 'max_distance', 'current_distance', 'type', 'id', 'orientation', 'covariance']
        ordered_fieldnames = [ 'time_boot_ms', 'min_distance', 'max_distance', 'current_distance', 'type', 'id', 'orientation', 'covariance' ]
        format = '<IHHHBBBB'
        native_format = bytearray('<IHHHBBBB', 'ascii')
        orders = [0, 1, 2, 3, 4, 5, 6, 7]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0]
        crc_extra = 85

        def __init__(self, time_boot_ms, min_distance, max_distance, current_distance, type, id, orientation, covariance):
                MAVLink_message.__init__(self, MAVLink_distance_sensor_message.id, MAVLink_distance_sensor_message.name)
                self._fieldnames = MAVLink_distance_sensor_message.fieldnames
                self.time_boot_ms = time_boot_ms
                self.min_distance = min_distance
                self.max_distance = max_distance
                self.current_distance = current_distance
                self.type = type
                self.id = id
                self.orientation = orientation
                self.covariance = covariance

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 85, struct.pack('<IHHHBBBB', self.time_boot_ms, self.min_distance, self.max_distance, self.current_distance, self.type, self.id, self.orientation, self.covariance))

class MAVLink_terrain_request_message(MAVLink_message):
        '''
        Request for terrain data and terrain status
        '''
        id = MAVLINK_MSG_ID_TERRAIN_REQUEST
        name = 'TERRAIN_REQUEST'
        fieldnames = ['lat', 'lon', 'grid_spacing', 'mask']
        ordered_fieldnames = [ 'mask', 'lat', 'lon', 'grid_spacing' ]
        format = '<QiiH'
        native_format = bytearray('<QiiH', 'ascii')
        orders = [1, 2, 3, 0]
        lengths = [1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0]
        crc_extra = 6

        def __init__(self, lat, lon, grid_spacing, mask):
                MAVLink_message.__init__(self, MAVLink_terrain_request_message.id, MAVLink_terrain_request_message.name)
                self._fieldnames = MAVLink_terrain_request_message.fieldnames
                self.lat = lat
                self.lon = lon
                self.grid_spacing = grid_spacing
                self.mask = mask

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 6, struct.pack('<QiiH', self.mask, self.lat, self.lon, self.grid_spacing))

class MAVLink_terrain_data_message(MAVLink_message):
        '''
        Terrain data sent from GCS. The lat/lon and grid_spacing must
        be the same as a lat/lon from a TERRAIN_REQUEST
        '''
        id = MAVLINK_MSG_ID_TERRAIN_DATA
        name = 'TERRAIN_DATA'
        fieldnames = ['lat', 'lon', 'grid_spacing', 'gridbit', 'data']
        ordered_fieldnames = [ 'lat', 'lon', 'grid_spacing', 'data', 'gridbit' ]
        format = '<iiH16hB'
        native_format = bytearray('<iiHhB', 'ascii')
        orders = [0, 1, 2, 4, 3]
        lengths = [1, 1, 1, 16, 1]
        array_lengths = [0, 0, 0, 16, 0]
        crc_extra = 229

        def __init__(self, lat, lon, grid_spacing, gridbit, data):
                MAVLink_message.__init__(self, MAVLink_terrain_data_message.id, MAVLink_terrain_data_message.name)
                self._fieldnames = MAVLink_terrain_data_message.fieldnames
                self.lat = lat
                self.lon = lon
                self.grid_spacing = grid_spacing
                self.gridbit = gridbit
                self.data = data

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 229, struct.pack('<iiH16hB', self.lat, self.lon, self.grid_spacing, self.data[0], self.data[1], self.data[2], self.data[3], self.data[4], self.data[5], self.data[6], self.data[7], self.data[8], self.data[9], self.data[10], self.data[11], self.data[12], self.data[13], self.data[14], self.data[15], self.gridbit))

class MAVLink_terrain_check_message(MAVLink_message):
        '''
        Request that the vehicle report terrain height at the given
        location. Used by GCS to check if vehicle has all terrain data
        needed for a mission.
        '''
        id = MAVLINK_MSG_ID_TERRAIN_CHECK
        name = 'TERRAIN_CHECK'
        fieldnames = ['lat', 'lon']
        ordered_fieldnames = [ 'lat', 'lon' ]
        format = '<ii'
        native_format = bytearray('<ii', 'ascii')
        orders = [0, 1]
        lengths = [1, 1]
        array_lengths = [0, 0]
        crc_extra = 203

        def __init__(self, lat, lon):
                MAVLink_message.__init__(self, MAVLink_terrain_check_message.id, MAVLink_terrain_check_message.name)
                self._fieldnames = MAVLink_terrain_check_message.fieldnames
                self.lat = lat
                self.lon = lon

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 203, struct.pack('<ii', self.lat, self.lon))

class MAVLink_terrain_report_message(MAVLink_message):
        '''
        Response from a TERRAIN_CHECK request
        '''
        id = MAVLINK_MSG_ID_TERRAIN_REPORT
        name = 'TERRAIN_REPORT'
        fieldnames = ['lat', 'lon', 'spacing', 'terrain_height', 'current_height', 'pending', 'loaded']
        ordered_fieldnames = [ 'lat', 'lon', 'terrain_height', 'current_height', 'spacing', 'pending', 'loaded' ]
        format = '<iiffHHH'
        native_format = bytearray('<iiffHHH', 'ascii')
        orders = [0, 1, 4, 2, 3, 5, 6]
        lengths = [1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0]
        crc_extra = 1

        def __init__(self, lat, lon, spacing, terrain_height, current_height, pending, loaded):
                MAVLink_message.__init__(self, MAVLink_terrain_report_message.id, MAVLink_terrain_report_message.name)
                self._fieldnames = MAVLink_terrain_report_message.fieldnames
                self.lat = lat
                self.lon = lon
                self.spacing = spacing
                self.terrain_height = terrain_height
                self.current_height = current_height
                self.pending = pending
                self.loaded = loaded

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 1, struct.pack('<iiffHHH', self.lat, self.lon, self.terrain_height, self.current_height, self.spacing, self.pending, self.loaded))

class MAVLink_scaled_pressure2_message(MAVLink_message):
        '''
        Barometer readings for 2nd barometer
        '''
        id = MAVLINK_MSG_ID_SCALED_PRESSURE2
        name = 'SCALED_PRESSURE2'
        fieldnames = ['time_boot_ms', 'press_abs', 'press_diff', 'temperature']
        ordered_fieldnames = [ 'time_boot_ms', 'press_abs', 'press_diff', 'temperature' ]
        format = '<Iffh'
        native_format = bytearray('<Iffh', 'ascii')
        orders = [0, 1, 2, 3]
        lengths = [1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0]
        crc_extra = 195

        def __init__(self, time_boot_ms, press_abs, press_diff, temperature):
                MAVLink_message.__init__(self, MAVLink_scaled_pressure2_message.id, MAVLink_scaled_pressure2_message.name)
                self._fieldnames = MAVLink_scaled_pressure2_message.fieldnames
                self.time_boot_ms = time_boot_ms
                self.press_abs = press_abs
                self.press_diff = press_diff
                self.temperature = temperature

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 195, struct.pack('<Iffh', self.time_boot_ms, self.press_abs, self.press_diff, self.temperature))

class MAVLink_att_pos_mocap_message(MAVLink_message):
        '''
        Motion capture attitude and position
        '''
        id = MAVLINK_MSG_ID_ATT_POS_MOCAP
        name = 'ATT_POS_MOCAP'
        fieldnames = ['time_usec', 'q', 'x', 'y', 'z']
        ordered_fieldnames = [ 'time_usec', 'q', 'x', 'y', 'z' ]
        format = '<Q4ffff'
        native_format = bytearray('<Qffff', 'ascii')
        orders = [0, 1, 2, 3, 4]
        lengths = [1, 4, 1, 1, 1]
        array_lengths = [0, 4, 0, 0, 0]
        crc_extra = 109

        def __init__(self, time_usec, q, x, y, z):
                MAVLink_message.__init__(self, MAVLink_att_pos_mocap_message.id, MAVLink_att_pos_mocap_message.name)
                self._fieldnames = MAVLink_att_pos_mocap_message.fieldnames
                self.time_usec = time_usec
                self.q = q
                self.x = x
                self.y = y
                self.z = z

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 109, struct.pack('<Q4ffff', self.time_usec, self.q[0], self.q[1], self.q[2], self.q[3], self.x, self.y, self.z))

class MAVLink_set_actuator_control_target_message(MAVLink_message):
        '''
        Set the vehicle attitude and body angular rates.
        '''
        id = MAVLINK_MSG_ID_SET_ACTUATOR_CONTROL_TARGET
        name = 'SET_ACTUATOR_CONTROL_TARGET'
        fieldnames = ['time_usec', 'group_mlx', 'target_system', 'target_component', 'controls']
        ordered_fieldnames = [ 'time_usec', 'controls', 'group_mlx', 'target_system', 'target_component' ]
        format = '<Q8fBBB'
        native_format = bytearray('<QfBBB', 'ascii')
        orders = [0, 2, 3, 4, 1]
        lengths = [1, 8, 1, 1, 1]
        array_lengths = [0, 8, 0, 0, 0]
        crc_extra = 168

        def __init__(self, time_usec, group_mlx, target_system, target_component, controls):
                MAVLink_message.__init__(self, MAVLink_set_actuator_control_target_message.id, MAVLink_set_actuator_control_target_message.name)
                self._fieldnames = MAVLink_set_actuator_control_target_message.fieldnames
                self.time_usec = time_usec
                self.group_mlx = group_mlx
                self.target_system = target_system
                self.target_component = target_component
                self.controls = controls

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 168, struct.pack('<Q8fBBB', self.time_usec, self.controls[0], self.controls[1], self.controls[2], self.controls[3], self.controls[4], self.controls[5], self.controls[6], self.controls[7], self.group_mlx, self.target_system, self.target_component))

class MAVLink_actuator_control_target_message(MAVLink_message):
        '''
        Set the vehicle attitude and body angular rates.
        '''
        id = MAVLINK_MSG_ID_ACTUATOR_CONTROL_TARGET
        name = 'ACTUATOR_CONTROL_TARGET'
        fieldnames = ['time_usec', 'group_mlx', 'controls']
        ordered_fieldnames = [ 'time_usec', 'controls', 'group_mlx' ]
        format = '<Q8fB'
        native_format = bytearray('<QfB', 'ascii')
        orders = [0, 2, 1]
        lengths = [1, 8, 1]
        array_lengths = [0, 8, 0]
        crc_extra = 181

        def __init__(self, time_usec, group_mlx, controls):
                MAVLink_message.__init__(self, MAVLink_actuator_control_target_message.id, MAVLink_actuator_control_target_message.name)
                self._fieldnames = MAVLink_actuator_control_target_message.fieldnames
                self.time_usec = time_usec
                self.group_mlx = group_mlx
                self.controls = controls

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 181, struct.pack('<Q8fB', self.time_usec, self.controls[0], self.controls[1], self.controls[2], self.controls[3], self.controls[4], self.controls[5], self.controls[6], self.controls[7], self.group_mlx))

class MAVLink_battery_status_message(MAVLink_message):
        '''
        Battery information
        '''
        id = MAVLINK_MSG_ID_BATTERY_STATUS
        name = 'BATTERY_STATUS'
        fieldnames = ['id', 'battery_function', 'type', 'temperature', 'voltages', 'current_battery', 'current_consumed', 'energy_consumed', 'battery_remaining']
        ordered_fieldnames = [ 'current_consumed', 'energy_consumed', 'temperature', 'voltages', 'current_battery', 'id', 'battery_function', 'type', 'battery_remaining' ]
        format = '<iih10HhBBBb'
        native_format = bytearray('<iihHhBBBb', 'ascii')
        orders = [5, 6, 7, 2, 3, 4, 0, 1, 8]
        lengths = [1, 1, 1, 10, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 10, 0, 0, 0, 0, 0]
        crc_extra = 154

        def __init__(self, id, battery_function, type, temperature, voltages, current_battery, current_consumed, energy_consumed, battery_remaining):
                MAVLink_message.__init__(self, MAVLink_battery_status_message.id, MAVLink_battery_status_message.name)
                self._fieldnames = MAVLink_battery_status_message.fieldnames
                self.id = id
                self.battery_function = battery_function
                self.type = type
                self.temperature = temperature
                self.voltages = voltages
                self.current_battery = current_battery
                self.current_consumed = current_consumed
                self.energy_consumed = energy_consumed
                self.battery_remaining = battery_remaining

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 154, struct.pack('<iih10HhBBBb', self.current_consumed, self.energy_consumed, self.temperature, self.voltages[0], self.voltages[1], self.voltages[2], self.voltages[3], self.voltages[4], self.voltages[5], self.voltages[6], self.voltages[7], self.voltages[8], self.voltages[9], self.current_battery, self.id, self.battery_function, self.type, self.battery_remaining))

class MAVLink_autopilot_version_message(MAVLink_message):
        '''
        Version and capability of autopilot software
        '''
        id = MAVLINK_MSG_ID_AUTOPILOT_VERSION
        name = 'AUTOPILOT_VERSION'
        fieldnames = ['capabilities', 'flight_sw_version', 'middleware_sw_version', 'os_sw_version', 'board_version', 'flight_custom_version', 'middleware_custom_version', 'os_custom_version', 'vendor_id', 'product_id', 'uid']
        ordered_fieldnames = [ 'capabilities', 'uid', 'flight_sw_version', 'middleware_sw_version', 'os_sw_version', 'board_version', 'vendor_id', 'product_id', 'flight_custom_version', 'middleware_custom_version', 'os_custom_version' ]
        format = '<QQIIIIHH8B8B8B'
        native_format = bytearray('<QQIIIIHHBBB', 'ascii')
        orders = [0, 2, 3, 4, 5, 8, 9, 10, 6, 7, 1]
        lengths = [1, 1, 1, 1, 1, 1, 1, 1, 8, 8, 8]
        array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 8, 8, 8]
        crc_extra = 178

        def __init__(self, capabilities, flight_sw_version, middleware_sw_version, os_sw_version, board_version, flight_custom_version, middleware_custom_version, os_custom_version, vendor_id, product_id, uid):
                MAVLink_message.__init__(self, MAVLink_autopilot_version_message.id, MAVLink_autopilot_version_message.name)
                self._fieldnames = MAVLink_autopilot_version_message.fieldnames
                self.capabilities = capabilities
                self.flight_sw_version = flight_sw_version
                self.middleware_sw_version = middleware_sw_version
                self.os_sw_version = os_sw_version
                self.board_version = board_version
                self.flight_custom_version = flight_custom_version
                self.middleware_custom_version = middleware_custom_version
                self.os_custom_version = os_custom_version
                self.vendor_id = vendor_id
                self.product_id = product_id
                self.uid = uid

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 178, struct.pack('<QQIIIIHH8B8B8B', self.capabilities, self.uid, self.flight_sw_version, self.middleware_sw_version, self.os_sw_version, self.board_version, self.vendor_id, self.product_id, self.flight_custom_version[0], self.flight_custom_version[1], self.flight_custom_version[2], self.flight_custom_version[3], self.flight_custom_version[4], self.flight_custom_version[5], self.flight_custom_version[6], self.flight_custom_version[7], self.middleware_custom_version[0], self.middleware_custom_version[1], self.middleware_custom_version[2], self.middleware_custom_version[3], self.middleware_custom_version[4], self.middleware_custom_version[5], self.middleware_custom_version[6], self.middleware_custom_version[7], self.os_custom_version[0], self.os_custom_version[1], self.os_custom_version[2], self.os_custom_version[3], self.os_custom_version[4], self.os_custom_version[5], self.os_custom_version[6], self.os_custom_version[7]))

class MAVLink_landing_target_message(MAVLink_message):
        '''
        The location of a landing area captured from a downward facing
        camera
        '''
        id = MAVLINK_MSG_ID_LANDING_TARGET
        name = 'LANDING_TARGET'
        fieldnames = ['target_num', 'frame', 'angle_x', 'angle_y', 'distance']
        ordered_fieldnames = [ 'angle_x', 'angle_y', 'distance', 'target_num', 'frame' ]
        format = '<fffBB'
        native_format = bytearray('<fffBB', 'ascii')
        orders = [3, 4, 0, 1, 2]
        lengths = [1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0]
        crc_extra = 255

        def __init__(self, target_num, frame, angle_x, angle_y, distance):
                MAVLink_message.__init__(self, MAVLink_landing_target_message.id, MAVLink_landing_target_message.name)
                self._fieldnames = MAVLink_landing_target_message.fieldnames
                self.target_num = target_num
                self.frame = frame
                self.angle_x = angle_x
                self.angle_y = angle_y
                self.distance = distance

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 255, struct.pack('<fffBB', self.angle_x, self.angle_y, self.distance, self.target_num, self.frame))

class MAVLink_vibration_message(MAVLink_message):
        '''
        Vibration levels and accelerometer clipping
        '''
        id = MAVLINK_MSG_ID_VIBRATION
        name = 'VIBRATION'
        fieldnames = ['time_usec', 'vibration_x', 'vibration_y', 'vibration_z', 'clipping_0', 'clipping_1', 'clipping_2']
        ordered_fieldnames = [ 'time_usec', 'vibration_x', 'vibration_y', 'vibration_z', 'clipping_0', 'clipping_1', 'clipping_2' ]
        format = '<QfffIII'
        native_format = bytearray('<QfffIII', 'ascii')
        orders = [0, 1, 2, 3, 4, 5, 6]
        lengths = [1, 1, 1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 0, 0, 0]
        crc_extra = 90

        def __init__(self, time_usec, vibration_x, vibration_y, vibration_z, clipping_0, clipping_1, clipping_2):
                MAVLink_message.__init__(self, MAVLink_vibration_message.id, MAVLink_vibration_message.name)
                self._fieldnames = MAVLink_vibration_message.fieldnames
                self.time_usec = time_usec
                self.vibration_x = vibration_x
                self.vibration_y = vibration_y
                self.vibration_z = vibration_z
                self.clipping_0 = clipping_0
                self.clipping_1 = clipping_1
                self.clipping_2 = clipping_2

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 90, struct.pack('<QfffIII', self.time_usec, self.vibration_x, self.vibration_y, self.vibration_z, self.clipping_0, self.clipping_1, self.clipping_2))

class MAVLink_v2_extension_message(MAVLink_message):
        '''
        Message implementing parts of the V2 payload specs in V1
        frames for transitional support.
        '''
        id = MAVLINK_MSG_ID_V2_EXTENSION
        name = 'V2_EXTENSION'
        fieldnames = ['target_network', 'target_system', 'target_component', 'message_type', 'payload']
        ordered_fieldnames = [ 'message_type', 'target_network', 'target_system', 'target_component', 'payload' ]
        format = '<HBBB249B'
        native_format = bytearray('<HBBBB', 'ascii')
        orders = [1, 2, 3, 0, 4]
        lengths = [1, 1, 1, 1, 249]
        array_lengths = [0, 0, 0, 0, 249]
        crc_extra = 8

        def __init__(self, target_network, target_system, target_component, message_type, payload):
                MAVLink_message.__init__(self, MAVLink_v2_extension_message.id, MAVLink_v2_extension_message.name)
                self._fieldnames = MAVLink_v2_extension_message.fieldnames
                self.target_network = target_network
                self.target_system = target_system
                self.target_component = target_component
                self.message_type = message_type
                self.payload = payload

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 8, struct.pack('<HBBB249B', self.message_type, self.target_network, self.target_system, self.target_component, self.payload[0], self.payload[1], self.payload[2], self.payload[3], self.payload[4], self.payload[5], self.payload[6], self.payload[7], self.payload[8], self.payload[9], self.payload[10], self.payload[11], self.payload[12], self.payload[13], self.payload[14], self.payload[15], self.payload[16], self.payload[17], self.payload[18], self.payload[19], self.payload[20], self.payload[21], self.payload[22], self.payload[23], self.payload[24], self.payload[25], self.payload[26], self.payload[27], self.payload[28], self.payload[29], self.payload[30], self.payload[31], self.payload[32], self.payload[33], self.payload[34], self.payload[35], self.payload[36], self.payload[37], self.payload[38], self.payload[39], self.payload[40], self.payload[41], self.payload[42], self.payload[43], self.payload[44], self.payload[45], self.payload[46], self.payload[47], self.payload[48], self.payload[49], self.payload[50], self.payload[51], self.payload[52], self.payload[53], self.payload[54], self.payload[55], self.payload[56], self.payload[57], self.payload[58], self.payload[59], self.payload[60], self.payload[61], self.payload[62], self.payload[63], self.payload[64], self.payload[65], self.payload[66], self.payload[67], self.payload[68], self.payload[69], self.payload[70], self.payload[71], self.payload[72], self.payload[73], self.payload[74], self.payload[75], self.payload[76], self.payload[77], self.payload[78], self.payload[79], self.payload[80], self.payload[81], self.payload[82], self.payload[83], self.payload[84], self.payload[85], self.payload[86], self.payload[87], self.payload[88], self.payload[89], self.payload[90], self.payload[91], self.payload[92], self.payload[93], self.payload[94], self.payload[95], self.payload[96], self.payload[97], self.payload[98], self.payload[99], self.payload[100], self.payload[101], self.payload[102], self.payload[103], self.payload[104], self.payload[105], self.payload[106], self.payload[107], self.payload[108], self.payload[109], self.payload[110], self.payload[111], self.payload[112], self.payload[113], self.payload[114], self.payload[115], self.payload[116], self.payload[117], self.payload[118], self.payload[119], self.payload[120], self.payload[121], self.payload[122], self.payload[123], self.payload[124], self.payload[125], self.payload[126], self.payload[127], self.payload[128], self.payload[129], self.payload[130], self.payload[131], self.payload[132], self.payload[133], self.payload[134], self.payload[135], self.payload[136], self.payload[137], self.payload[138], self.payload[139], self.payload[140], self.payload[141], self.payload[142], self.payload[143], self.payload[144], self.payload[145], self.payload[146], self.payload[147], self.payload[148], self.payload[149], self.payload[150], self.payload[151], self.payload[152], self.payload[153], self.payload[154], self.payload[155], self.payload[156], self.payload[157], self.payload[158], self.payload[159], self.payload[160], self.payload[161], self.payload[162], self.payload[163], self.payload[164], self.payload[165], self.payload[166], self.payload[167], self.payload[168], self.payload[169], self.payload[170], self.payload[171], self.payload[172], self.payload[173], self.payload[174], self.payload[175], self.payload[176], self.payload[177], self.payload[178], self.payload[179], self.payload[180], self.payload[181], self.payload[182], self.payload[183], self.payload[184], self.payload[185], self.payload[186], self.payload[187], self.payload[188], self.payload[189], self.payload[190], self.payload[191], self.payload[192], self.payload[193], self.payload[194], self.payload[195], self.payload[196], self.payload[197], self.payload[198], self.payload[199], self.payload[200], self.payload[201], self.payload[202], self.payload[203], self.payload[204], self.payload[205], self.payload[206], self.payload[207], self.payload[208], self.payload[209], self.payload[210], self.payload[211], self.payload[212], self.payload[213], self.payload[214], self.payload[215], self.payload[216], self.payload[217], self.payload[218], self.payload[219], self.payload[220], self.payload[221], self.payload[222], self.payload[223], self.payload[224], self.payload[225], self.payload[226], self.payload[227], self.payload[228], self.payload[229], self.payload[230], self.payload[231], self.payload[232], self.payload[233], self.payload[234], self.payload[235], self.payload[236], self.payload[237], self.payload[238], self.payload[239], self.payload[240], self.payload[241], self.payload[242], self.payload[243], self.payload[244], self.payload[245], self.payload[246], self.payload[247], self.payload[248]))

class MAVLink_memory_vect_message(MAVLink_message):
        '''
        Send raw controller memory. The use of this message is
        discouraged for normal packets, but a quite efficient way for
        testing new messages and getting experimental debug output.
        '''
        id = MAVLINK_MSG_ID_MEMORY_VECT
        name = 'MEMORY_VECT'
        fieldnames = ['address', 'ver', 'type', 'value']
        ordered_fieldnames = [ 'address', 'ver', 'type', 'value' ]
        format = '<HBB32b'
        native_format = bytearray('<HBBb', 'ascii')
        orders = [0, 1, 2, 3]
        lengths = [1, 1, 1, 32]
        array_lengths = [0, 0, 0, 32]
        crc_extra = 204

        def __init__(self, address, ver, type, value):
                MAVLink_message.__init__(self, MAVLink_memory_vect_message.id, MAVLink_memory_vect_message.name)
                self._fieldnames = MAVLink_memory_vect_message.fieldnames
                self.address = address
                self.ver = ver
                self.type = type
                self.value = value

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 204, struct.pack('<HBB32b', self.address, self.ver, self.type, self.value[0], self.value[1], self.value[2], self.value[3], self.value[4], self.value[5], self.value[6], self.value[7], self.value[8], self.value[9], self.value[10], self.value[11], self.value[12], self.value[13], self.value[14], self.value[15], self.value[16], self.value[17], self.value[18], self.value[19], self.value[20], self.value[21], self.value[22], self.value[23], self.value[24], self.value[25], self.value[26], self.value[27], self.value[28], self.value[29], self.value[30], self.value[31]))

class MAVLink_debug_vect_message(MAVLink_message):
        '''

        '''
        id = MAVLINK_MSG_ID_DEBUG_VECT
        name = 'DEBUG_VECT'
        fieldnames = ['name', 'time_usec', 'x', 'y', 'z']
        ordered_fieldnames = [ 'time_usec', 'x', 'y', 'z', 'name' ]
        format = '<Qfff10s'
        native_format = bytearray('<Qfffc', 'ascii')
        orders = [4, 0, 1, 2, 3]
        lengths = [1, 1, 1, 1, 1]
        array_lengths = [0, 0, 0, 0, 10]
        crc_extra = 49

        def __init__(self, name, time_usec, x, y, z):
                MAVLink_message.__init__(self, MAVLink_debug_vect_message.id, MAVLink_debug_vect_message.name)
                self._fieldnames = MAVLink_debug_vect_message.fieldnames
                self.name = name
                self.time_usec = time_usec
                self.x = x
                self.y = y
                self.z = z

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 49, struct.pack('<Qfff10s', self.time_usec, self.x, self.y, self.z, self.name))

class MAVLink_named_value_float_message(MAVLink_message):
        '''
        Send a key-value pair as float. The use of this message is
        discouraged for normal packets, but a quite efficient way for
        testing new messages and getting experimental debug output.
        '''
        id = MAVLINK_MSG_ID_NAMED_VALUE_FLOAT
        name = 'NAMED_VALUE_FLOAT'
        fieldnames = ['time_boot_ms', 'name', 'value']
        ordered_fieldnames = [ 'time_boot_ms', 'value', 'name' ]
        format = '<If10s'
        native_format = bytearray('<Ifc', 'ascii')
        orders = [0, 2, 1]
        lengths = [1, 1, 1]
        array_lengths = [0, 0, 10]
        crc_extra = 170

        def __init__(self, time_boot_ms, name, value):
                MAVLink_message.__init__(self, MAVLink_named_value_float_message.id, MAVLink_named_value_float_message.name)
                self._fieldnames = MAVLink_named_value_float_message.fieldnames
                self.time_boot_ms = time_boot_ms
                self.name = name
                self.value = value

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 170, struct.pack('<If10s', self.time_boot_ms, self.value, self.name))

class MAVLink_named_value_int_message(MAVLink_message):
        '''
        Send a key-value pair as integer. The use of this message is
        discouraged for normal packets, but a quite efficient way for
        testing new messages and getting experimental debug output.
        '''
        id = MAVLINK_MSG_ID_NAMED_VALUE_INT
        name = 'NAMED_VALUE_INT'
        fieldnames = ['time_boot_ms', 'name', 'value']
        ordered_fieldnames = [ 'time_boot_ms', 'value', 'name' ]
        format = '<Ii10s'
        native_format = bytearray('<Iic', 'ascii')
        orders = [0, 2, 1]
        lengths = [1, 1, 1]
        array_lengths = [0, 0, 10]
        crc_extra = 44

        def __init__(self, time_boot_ms, name, value):
                MAVLink_message.__init__(self, MAVLink_named_value_int_message.id, MAVLink_named_value_int_message.name)
                self._fieldnames = MAVLink_named_value_int_message.fieldnames
                self.time_boot_ms = time_boot_ms
                self.name = name
                self.value = value

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 44, struct.pack('<Ii10s', self.time_boot_ms, self.value, self.name))

class MAVLink_statustext_message(MAVLink_message):
        '''
        Status text message. These messages are printed in yellow in
        the COMM console of QGroundControl. WARNING: They consume
        quite some bandwidth, so use only for important status and
        error messages. If implemented wisely, these messages are
        buffered on the MCU and sent only at a limited rate (e.g. 10
        Hz).
        '''
        id = MAVLINK_MSG_ID_STATUSTEXT
        name = 'STATUSTEXT'
        fieldnames = ['severity', 'text']
        ordered_fieldnames = [ 'severity', 'text' ]
        format = '<B50s'
        native_format = bytearray('<Bc', 'ascii')
        orders = [0, 1]
        lengths = [1, 1]
        array_lengths = [0, 50]
        crc_extra = 83

        def __init__(self, severity, text):
                MAVLink_message.__init__(self, MAVLink_statustext_message.id, MAVLink_statustext_message.name)
                self._fieldnames = MAVLink_statustext_message.fieldnames
                self.severity = severity
                self.text = text

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 83, struct.pack('<B50s', self.severity, self.text))

class MAVLink_debug_message(MAVLink_message):
        '''
        Send a debug value. The index is used to discriminate between
        values. These values show up in the plot of QGroundControl as
        DEBUG N.
        '''
        id = MAVLINK_MSG_ID_DEBUG
        name = 'DEBUG'
        fieldnames = ['time_boot_ms', 'ind', 'value']
        ordered_fieldnames = [ 'time_boot_ms', 'value', 'ind' ]
        format = '<IfB'
        native_format = bytearray('<IfB', 'ascii')
        orders = [0, 2, 1]
        lengths = [1, 1, 1]
        array_lengths = [0, 0, 0]
        crc_extra = 46

        def __init__(self, time_boot_ms, ind, value):
                MAVLink_message.__init__(self, MAVLink_debug_message.id, MAVLink_debug_message.name)
                self._fieldnames = MAVLink_debug_message.fieldnames
                self.time_boot_ms = time_boot_ms
                self.ind = ind
                self.value = value

        def pack(self, mav):
                return MAVLink_message.pack(self, mav, 46, struct.pack('<IfB', self.time_boot_ms, self.value, self.ind))


mavlink_map = {
        MAVLINK_MSG_ID_HEARTBEAT : MAVLink_heartbeat_message,
        MAVLINK_MSG_ID_SYS_STATUS : MAVLink_sys_status_message,
        MAVLINK_MSG_ID_SYSTEM_TIME : MAVLink_system_time_message,
        MAVLINK_MSG_ID_PING : MAVLink_ping_message,
        MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL : MAVLink_change_operator_control_message,
        MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL_ACK : MAVLink_change_operator_control_ack_message,
        MAVLINK_MSG_ID_AUTH_KEY : MAVLink_auth_key_message,
        MAVLINK_MSG_ID_SET_MODE : MAVLink_set_mode_message,
        MAVLINK_MSG_ID_PARAM_REQUEST_READ : MAVLink_param_request_read_message,
        MAVLINK_MSG_ID_PARAM_REQUEST_LIST : MAVLink_param_request_list_message,
        MAVLINK_MSG_ID_PARAM_VALUE : MAVLink_param_value_message,
        MAVLINK_MSG_ID_PARAM_SET : MAVLink_param_set_message,
        MAVLINK_MSG_ID_GPS_RAW_INT : MAVLink_gps_raw_int_message,
        MAVLINK_MSG_ID_GPS_STATUS : MAVLink_gps_status_message,
        MAVLINK_MSG_ID_SCALED_IMU : MAVLink_scaled_imu_message,
        MAVLINK_MSG_ID_RAW_IMU : MAVLink_raw_imu_message,
        MAVLINK_MSG_ID_RAW_PRESSURE : MAVLink_raw_pressure_message,
        MAVLINK_MSG_ID_SCALED_PRESSURE : MAVLink_scaled_pressure_message,
        MAVLINK_MSG_ID_ATTITUDE : MAVLink_attitude_message,
        MAVLINK_MSG_ID_ATTITUDE_QUATERNION : MAVLink_attitude_quaternion_message,
        MAVLINK_MSG_ID_LOCAL_POSITION_NED : MAVLink_local_position_ned_message,
        MAVLINK_MSG_ID_GLOBAL_POSITION_INT : MAVLink_global_position_int_message,
        MAVLINK_MSG_ID_RC_CHANNELS_SCALED : MAVLink_rc_channels_scaled_message,
        MAVLINK_MSG_ID_RC_CHANNELS_RAW : MAVLink_rc_channels_raw_message,
        MAVLINK_MSG_ID_SERVO_OUTPUT_RAW : MAVLink_servo_output_raw_message,
        MAVLINK_MSG_ID_MISSION_REQUEST_PARTIAL_LIST : MAVLink_mission_request_partial_list_message,
        MAVLINK_MSG_ID_MISSION_WRITE_PARTIAL_LIST : MAVLink_mission_write_partial_list_message,
        MAVLINK_MSG_ID_MISSION_ITEM : MAVLink_mission_item_message,
        MAVLINK_MSG_ID_MISSION_REQUEST : MAVLink_mission_request_message,
        MAVLINK_MSG_ID_MISSION_SET_CURRENT : MAVLink_mission_set_current_message,
        MAVLINK_MSG_ID_MISSION_CURRENT : MAVLink_mission_current_message,
        MAVLINK_MSG_ID_MISSION_REQUEST_LIST : MAVLink_mission_request_list_message,
        MAVLINK_MSG_ID_MISSION_COUNT : MAVLink_mission_count_message,
        MAVLINK_MSG_ID_MISSION_CLEAR_ALL : MAVLink_mission_clear_all_message,
        MAVLINK_MSG_ID_MISSION_ITEM_REACHED : MAVLink_mission_item_reached_message,
        MAVLINK_MSG_ID_MISSION_ACK : MAVLink_mission_ack_message,
        MAVLINK_MSG_ID_SET_GPS_GLOBAL_ORIGIN : MAVLink_set_gps_global_origin_message,
        MAVLINK_MSG_ID_GPS_GLOBAL_ORIGIN : MAVLink_gps_global_origin_message,
        MAVLINK_MSG_ID_PARAM_MAP_RC : MAVLink_param_map_rc_message,
        MAVLINK_MSG_ID_SAFETY_SET_ALLOWED_AREA : MAVLink_safety_set_allowed_area_message,
        MAVLINK_MSG_ID_SAFETY_ALLOWED_AREA : MAVLink_safety_allowed_area_message,
        MAVLINK_MSG_ID_ATTITUDE_QUATERNION_COV : MAVLink_attitude_quaternion_cov_message,
        MAVLINK_MSG_ID_NAV_CONTROLLER_OUTPUT : MAVLink_nav_controller_output_message,
        MAVLINK_MSG_ID_GLOBAL_POSITION_INT_COV : MAVLink_global_position_int_cov_message,
        MAVLINK_MSG_ID_LOCAL_POSITION_NED_COV : MAVLink_local_position_ned_cov_message,
        MAVLINK_MSG_ID_RC_CHANNELS : MAVLink_rc_channels_message,
        MAVLINK_MSG_ID_REQUEST_DATA_STREAM : MAVLink_request_data_stream_message,
        MAVLINK_MSG_ID_DATA_STREAM : MAVLink_data_stream_message,
        MAVLINK_MSG_ID_MANUAL_CONTROL : MAVLink_manual_control_message,
        MAVLINK_MSG_ID_RC_CHANNELS_OVERRIDE : MAVLink_rc_channels_override_message,
        MAVLINK_MSG_ID_MISSION_ITEM_INT : MAVLink_mission_item_int_message,
        MAVLINK_MSG_ID_VFR_HUD : MAVLink_vfr_hud_message,
        MAVLINK_MSG_ID_COMMAND_INT : MAVLink_command_int_message,
        MAVLINK_MSG_ID_COMMAND_LONG : MAVLink_command_long_message,
        MAVLINK_MSG_ID_COMMAND_ACK : MAVLink_command_ack_message,
        MAVLINK_MSG_ID_MANUAL_SETPOINT : MAVLink_manual_setpoint_message,
        MAVLINK_MSG_ID_SET_ATTITUDE_TARGET : MAVLink_set_attitude_target_message,
        MAVLINK_MSG_ID_ATTITUDE_TARGET : MAVLink_attitude_target_message,
        MAVLINK_MSG_ID_SET_POSITION_TARGET_LOCAL_NED : MAVLink_set_position_target_local_ned_message,
        MAVLINK_MSG_ID_POSITION_TARGET_LOCAL_NED : MAVLink_position_target_local_ned_message,
        MAVLINK_MSG_ID_SET_POSITION_TARGET_GLOBAL_INT : MAVLink_set_position_target_global_int_message,
        MAVLINK_MSG_ID_POSITION_TARGET_GLOBAL_INT : MAVLink_position_target_global_int_message,
        MAVLINK_MSG_ID_LOCAL_POSITION_NED_SYSTEM_GLOBAL_OFFSET : MAVLink_local_position_ned_system_global_offset_message,
        MAVLINK_MSG_ID_HIL_STATE : MAVLink_hil_state_message,
        MAVLINK_MSG_ID_HIL_CONTROLS : MAVLink_hil_controls_message,
        MAVLINK_MSG_ID_HIL_RC_INPUTS_RAW : MAVLink_hil_rc_inputs_raw_message,
        MAVLINK_MSG_ID_OPTICAL_FLOW : MAVLink_optical_flow_message,
        MAVLINK_MSG_ID_GLOBAL_VISION_POSITION_ESTIMATE : MAVLink_global_vision_position_estimate_message,
        MAVLINK_MSG_ID_VISION_POSITION_ESTIMATE : MAVLink_vision_position_estimate_message,
        MAVLINK_MSG_ID_VISION_SPEED_ESTIMATE : MAVLink_vision_speed_estimate_message,
        MAVLINK_MSG_ID_VICON_POSITION_ESTIMATE : MAVLink_vicon_position_estimate_message,
        MAVLINK_MSG_ID_HIGHRES_IMU : MAVLink_highres_imu_message,
        MAVLINK_MSG_ID_OPTICAL_FLOW_RAD : MAVLink_optical_flow_rad_message,
        MAVLINK_MSG_ID_HIL_SENSOR : MAVLink_hil_sensor_message,
        MAVLINK_MSG_ID_SIM_STATE : MAVLink_sim_state_message,
        MAVLINK_MSG_ID_RADIO_STATUS : MAVLink_radio_status_message,
        MAVLINK_MSG_ID_FILE_TRANSFER_PROTOCOL : MAVLink_file_transfer_protocol_message,
        MAVLINK_MSG_ID_TIMESYNC : MAVLink_timesync_message,
        MAVLINK_MSG_ID_CAMERA_TRIGGER : MAVLink_camera_trigger_message,
        MAVLINK_MSG_ID_HIL_GPS : MAVLink_hil_gps_message,
        MAVLINK_MSG_ID_HIL_OPTICAL_FLOW : MAVLink_hil_optical_flow_message,
        MAVLINK_MSG_ID_HIL_STATE_QUATERNION : MAVLink_hil_state_quaternion_message,
        MAVLINK_MSG_ID_SCALED_IMU2 : MAVLink_scaled_imu2_message,
        MAVLINK_MSG_ID_LOG_REQUEST_LIST : MAVLink_log_request_list_message,
        MAVLINK_MSG_ID_LOG_ENTRY : MAVLink_log_entry_message,
        MAVLINK_MSG_ID_LOG_REQUEST_DATA : MAVLink_log_request_data_message,
        MAVLINK_MSG_ID_LOG_DATA : MAVLink_log_data_message,
        MAVLINK_MSG_ID_LOG_ERASE : MAVLink_log_erase_message,
        MAVLINK_MSG_ID_LOG_REQUEST_END : MAVLink_log_request_end_message,
        MAVLINK_MSG_ID_GPS_INJECT_DATA : MAVLink_gps_inject_data_message,
        MAVLINK_MSG_ID_GPS2_RAW : MAVLink_gps2_raw_message,
        MAVLINK_MSG_ID_POWER_STATUS : MAVLink_power_status_message,
        MAVLINK_MSG_ID_SERIAL_CONTROL : MAVLink_serial_control_message,
        MAVLINK_MSG_ID_GPS_RTK : MAVLink_gps_rtk_message,
        MAVLINK_MSG_ID_GPS2_RTK : MAVLink_gps2_rtk_message,
        MAVLINK_MSG_ID_SCALED_IMU3 : MAVLink_scaled_imu3_message,
        MAVLINK_MSG_ID_DATA_TRANSMISSION_HANDSHAKE : MAVLink_data_transmission_handshake_message,
        MAVLINK_MSG_ID_ENCAPSULATED_DATA : MAVLink_encapsulated_data_message,
        MAVLINK_MSG_ID_DISTANCE_SENSOR : MAVLink_distance_sensor_message,
        MAVLINK_MSG_ID_TERRAIN_REQUEST : MAVLink_terrain_request_message,
        MAVLINK_MSG_ID_TERRAIN_DATA : MAVLink_terrain_data_message,
        MAVLINK_MSG_ID_TERRAIN_CHECK : MAVLink_terrain_check_message,
        MAVLINK_MSG_ID_TERRAIN_REPORT : MAVLink_terrain_report_message,
        MAVLINK_MSG_ID_SCALED_PRESSURE2 : MAVLink_scaled_pressure2_message,
        MAVLINK_MSG_ID_ATT_POS_MOCAP : MAVLink_att_pos_mocap_message,
        MAVLINK_MSG_ID_SET_ACTUATOR_CONTROL_TARGET : MAVLink_set_actuator_control_target_message,
        MAVLINK_MSG_ID_ACTUATOR_CONTROL_TARGET : MAVLink_actuator_control_target_message,
        MAVLINK_MSG_ID_BATTERY_STATUS : MAVLink_battery_status_message,
        MAVLINK_MSG_ID_AUTOPILOT_VERSION : MAVLink_autopilot_version_message,
        MAVLINK_MSG_ID_LANDING_TARGET : MAVLink_landing_target_message,
        MAVLINK_MSG_ID_VIBRATION : MAVLink_vibration_message,
        MAVLINK_MSG_ID_V2_EXTENSION : MAVLink_v2_extension_message,
        MAVLINK_MSG_ID_MEMORY_VECT : MAVLink_memory_vect_message,
        MAVLINK_MSG_ID_DEBUG_VECT : MAVLink_debug_vect_message,
        MAVLINK_MSG_ID_NAMED_VALUE_FLOAT : MAVLink_named_value_float_message,
        MAVLINK_MSG_ID_NAMED_VALUE_INT : MAVLink_named_value_int_message,
        MAVLINK_MSG_ID_STATUSTEXT : MAVLink_statustext_message,
        MAVLINK_MSG_ID_DEBUG : MAVLink_debug_message,
}

class MAVError(Exception):
        '''MAVLink error class'''
        def __init__(self, msg):
            Exception.__init__(self, msg)
            self.message = msg

class MAVString(str):
        '''NUL terminated string'''
        def __init__(self, s):
                str.__init__(self)
        def __str__(self):
            i = self.find(chr(0))
            if i == -1:
                return self[:]
            return self[0:i]

class MAVLink_bad_data(MAVLink_message):
        '''
        a piece of bad data in a mavlink stream
        '''
        def __init__(self, data, reason):
                MAVLink_message.__init__(self, MAVLINK_MSG_ID_BAD_DATA, 'BAD_DATA')
                self._fieldnames = ['data', 'reason']
                self.data = data
                self.reason = reason
                self._msgbuf = data

        def __str__(self):
            '''Override the __str__ function from MAVLink_messages because non-printable characters are common in to be the reason for this message to exist.'''
            return '%s {%s, data:%s}' % (self._type, self.reason, [('%x' % ord(i) if isinstance(i, str) else '%x' % i) for i in self.data])

class MAVLink(object):
        '''MAVLink protocol handling class'''
        def __init__(self, file, srcSystem=0, srcComponent=0, use_native=False):
                self.seq = 0
                self.file = file
                self.srcSystem = srcSystem
                self.srcComponent = srcComponent
                self.callback = None
                self.callback_args = None
                self.callback_kwargs = None
                self.send_callback = None
                self.send_callback_args = None
                self.send_callback_kwargs = None
                self.buf = bytearray()
                self.expected_length = 8
                self.have_prefix_error = False
                self.robust_parsing = False
                self.protocol_marker = 254
                self.little_endian = True
                self.crc_extra = True
                self.sort_fields = True
                self.total_packets_sent = 0
                self.total_bytes_sent = 0
                self.total_packets_received = 0
                self.total_bytes_received = 0
                self.total_receive_errors = 0
                self.startup_time = time.time()
                if native_supported and (use_native or native_testing or native_force):
                    print("NOTE: mavnative is currently beta-test code")
                    self.native = mavnative.NativeConnection(MAVLink_message, mavlink_map)
                else:
                    self.native = None
                if native_testing:
                    self.test_buf = bytearray()

        def set_callback(self, callback, *args, **kwargs):
            self.callback = callback
            self.callback_args = args
            self.callback_kwargs = kwargs

        def set_send_callback(self, callback, *args, **kwargs):
            self.send_callback = callback
            self.send_callback_args = args
            self.send_callback_kwargs = kwargs

        def send(self, mavmsg):
                '''send a MAVLink message'''
                buf = mavmsg.pack(self)
                self.file.write(buf)
                self.seq = (self.seq + 1) % 256
                self.total_packets_sent += 1
                self.total_bytes_sent += len(buf)
                if self.send_callback:
                    self.send_callback(mavmsg, *self.send_callback_args, **self.send_callback_kwargs)

        def bytes_needed(self):
            '''return number of bytes needed for next parsing stage'''
            if self.native:
                ret = self.native.expected_length - len(self.buf)
            else:
                ret = self.expected_length - len(self.buf)
            
            if ret <= 0:
                return 1
            return ret

        def __parse_char_native(self, c):
            '''this method exists only to see in profiling results'''
            m = self.native.parse_chars(c)
            return m

        def __callbacks(self, msg):
            '''this method exists only to make profiling results easier to read'''
            if self.callback:
                self.callback(msg, *self.callback_args, **self.callback_kwargs)

        def parse_char(self, c):
            '''input some data bytes, possibly returning a new message'''
            self.buf.extend(c)

            self.total_bytes_received += len(c)

            if self.native:
                if native_testing:
                    self.test_buf.extend(c)
                    m = self.__parse_char_native(self.test_buf)
                    m2 = self.__parse_char_legacy()
                    if m2 != m:
                        print("Native: %s\nLegacy: %s\n" % (m, m2))
                        raise Exception('Native vs. Legacy mismatch')
                else:
                    m = self.__parse_char_native(self.buf)
            else:
                m = self.__parse_char_legacy()

            if m != None:
                self.total_packets_received += 1
                self.__callbacks(m)

            return m

        def __parse_char_legacy(self):
            '''input some data bytes, possibly returning a new message (uses no native code)'''
            if len(self.buf) >= 1 and self.buf[0] != 254:
                magic = self.buf[0]
                self.buf = self.buf[1:]
                if self.robust_parsing:
                    m = MAVLink_bad_data(chr(magic), "Bad prefix")
                    self.expected_length = 8
                    self.total_receive_errors += 1
                    return m
                if self.have_prefix_error:
                    return None
                self.have_prefix_error = True
                self.total_receive_errors += 1
                raise MAVError("invalid MAVLink prefix '%s'" % magic)
            self.have_prefix_error = False
            if len(self.buf) >= 2:
                if sys.version_info[0] < 3:
                    (magic, self.expected_length) = struct.unpack('BB', str(self.buf[0:2])) # bytearrays are not supported in py 2.7.3
                else:
                    (magic, self.expected_length) = struct.unpack('BB', self.buf[0:2])
                self.expected_length += 8
            if self.expected_length >= 8 and len(self.buf) >= self.expected_length:
                mbuf = array.array('B', self.buf[0:self.expected_length])
                self.buf = self.buf[self.expected_length:]
                self.expected_length = 8
                if self.robust_parsing:
                    try:
                        m = self.decode(mbuf)
                    except MAVError as reason:
                        m = MAVLink_bad_data(mbuf, reason.message)
                        self.total_receive_errors += 1
                else:
                    m = self.decode(mbuf)
                return m
            return None

        def parse_buffer(self, s):
            '''input some data bytes, possibly returning a list of new messages'''
            m = self.parse_char(s)
            if m is None:
                return None
            ret = [m]
            while True:
                m = self.parse_char("")
                if m is None:
                    return ret
                ret.append(m)
            return ret

        def decode(self, msgbuf):
                '''decode a buffer as a MAVLink message'''
                # decode the header
                try:
                    magic, mlen, seq, srcSystem, srcComponent, msgId = struct.unpack('cBBBBB', msgbuf[:6])
                except struct.error as emsg:
                    raise MAVError('Unable to unpack MAVLink header: %s' % emsg)
                if ord(magic) != 254:
                    raise MAVError("invalid MAVLink prefix '%s'" % magic)
                if mlen != len(msgbuf)-8:
                    raise MAVError('invalid MAVLink message length. Got %u expected %u, msgId=%u' % (len(msgbuf)-8, mlen, msgId))

                if not msgId in mavlink_map:
                    raise MAVError('unknown MAVLink message ID %u' % msgId)

                # decode the payload
                type = mavlink_map[msgId]
                fmt = type.format
                order_map = type.orders
                len_map = type.lengths
                crc_extra = type.crc_extra

                # decode the checksum
                try:
                    crc, = struct.unpack('<H', msgbuf[-2:])
                except struct.error as emsg:
                    raise MAVError('Unable to unpack MAVLink CRC: %s' % emsg)
                crcbuf = msgbuf[1:-2]
                if True: # using CRC extra
                    crcbuf.append(crc_extra)
                crc2 = x25crc(crcbuf)
                if crc != crc2.crc:
                    raise MAVError('invalid MAVLink CRC in msgID %u 0x%04x should be 0x%04x' % (msgId, crc, crc2.crc))

                try:
                    t = struct.unpack(fmt, msgbuf[6:-2])
                except struct.error as emsg:
                    raise MAVError('Unable to unpack MAVLink payload type=%s fmt=%s payloadLength=%u: %s' % (
                        type, fmt, len(msgbuf[6:-2]), emsg))

                tlist = list(t)
                # handle sorted fields
                if True:
                    t = tlist[:]
                    if sum(len_map) == len(len_map):
                        # message has no arrays in it
                        for i in range(0, len(tlist)):
                            tlist[i] = t[order_map[i]]
                    else:
                        # message has some arrays
                        tlist = []
                        for i in range(0, len(order_map)):
                            order = order_map[i]
                            L = len_map[order]
                            tip = sum(len_map[:order])
                            field = t[tip]
                            if L == 1 or isinstance(field, str):
                                tlist.append(field)
                            else:
                                tlist.append(t[tip:(tip + L)])

                # terminate any strings
                for i in range(0, len(tlist)):
                    if isinstance(tlist[i], str):
                        tlist[i] = str(MAVString(tlist[i]))
                t = tuple(tlist)
                # construct the message object
                try:
                    m = type(*t)
                except Exception as emsg:
                    raise MAVError('Unable to instantiate MAVLink message of type %s : %s' % (type, emsg))
                m._msgbuf = msgbuf
                m._payload = msgbuf[6:-2]
                m._crc = crc
                m._header = MAVLink_header(msgId, mlen, seq, srcSystem, srcComponent)
                return m
        def heartbeat_encode(self, type, autopilot, base_mode, custom_mode, system_status, mavlink_version=3):
                '''
                The heartbeat message shows that a system is present and responding.
                The type of the MAV and Autopilot hardware allow the
                receiving system to treat further messages from this
                system appropriate (e.g. by laying out the user
                interface based on the autopilot).

                type                      : Type of the MAV (quadrotor, helicopter, etc., up to 15 types, defined in MAV_TYPE ENUM) (uint8_t)
                autopilot                 : Autopilot type / class. defined in MAV_AUTOPILOT ENUM (uint8_t)
                base_mode                 : System mode bitfield, see MAV_MODE_FLAG ENUM in mavlink/include/mavlink_types.h (uint8_t)
                custom_mode               : A bitfield for use for autopilot-specific flags. (uint32_t)
                system_status             : System status flag, see MAV_STATE ENUM (uint8_t)
                mavlink_version           : MAVLink version, not writable by user, gets added by protocol because of magic data type: uint8_t_mavlink_version (uint8_t)

                '''
                return MAVLink_heartbeat_message(type, autopilot, base_mode, custom_mode, system_status, mavlink_version)

        def heartbeat_send(self, type, autopilot, base_mode, custom_mode, system_status, mavlink_version=3):
                '''
                The heartbeat message shows that a system is present and responding.
                The type of the MAV and Autopilot hardware allow the
                receiving system to treat further messages from this
                system appropriate (e.g. by laying out the user
                interface based on the autopilot).

                type                      : Type of the MAV (quadrotor, helicopter, etc., up to 15 types, defined in MAV_TYPE ENUM) (uint8_t)
                autopilot                 : Autopilot type / class. defined in MAV_AUTOPILOT ENUM (uint8_t)
                base_mode                 : System mode bitfield, see MAV_MODE_FLAG ENUM in mavlink/include/mavlink_types.h (uint8_t)
                custom_mode               : A bitfield for use for autopilot-specific flags. (uint32_t)
                system_status             : System status flag, see MAV_STATE ENUM (uint8_t)
                mavlink_version           : MAVLink version, not writable by user, gets added by protocol because of magic data type: uint8_t_mavlink_version (uint8_t)

                '''
                return self.send(self.heartbeat_encode(type, autopilot, base_mode, custom_mode, system_status, mavlink_version))

        def sys_status_encode(self, onboard_control_sensors_present, onboard_control_sensors_enabled, onboard_control_sensors_health, load, voltage_battery, current_battery, battery_remaining, drop_rate_comm, errors_comm, errors_count1, errors_count2, errors_count3, errors_count4):
                '''
                The general system state. If the system is following the MAVLink
                standard, the system state is mainly defined by three
                orthogonal states/modes: The system mode, which is
                either LOCKED (motors shut down and locked), MANUAL
                (system under RC control), GUIDED (system with
                autonomous position control, position setpoint
                controlled manually) or AUTO (system guided by
                path/waypoint planner). The NAV_MODE defined the
                current flight state: LIFTOFF (often an open-loop
                maneuver), LANDING, WAYPOINTS or VECTOR. This
                represents the internal navigation state machine. The
                system status shows wether the system is currently
                active or not and if an emergency occured. During the
                CRITICAL and EMERGENCY states the MAV is still
                considered to be active, but should start emergency
                procedures autonomously. After a failure occured it
                should first move from active to critical to allow
                manual intervention and then move to emergency after a
                certain timeout.

                onboard_control_sensors_present        : Bitmask showing which onboard controllers and sensors are present. Value of 0: not present. Value of 1: present. Indices defined by ENUM MAV_SYS_STATUS_SENSOR (uint32_t)
                onboard_control_sensors_enabled        : Bitmask showing which onboard controllers and sensors are enabled:  Value of 0: not enabled. Value of 1: enabled. Indices defined by ENUM MAV_SYS_STATUS_SENSOR (uint32_t)
                onboard_control_sensors_health        : Bitmask showing which onboard controllers and sensors are operational or have an error:  Value of 0: not enabled. Value of 1: enabled. Indices defined by ENUM MAV_SYS_STATUS_SENSOR (uint32_t)
                load                      : Maximum usage in percent of the mainloop time, (0%: 0, 100%: 1000) should be always below 1000 (uint16_t)
                voltage_battery           : Battery voltage, in millivolts (1 = 1 millivolt) (uint16_t)
                current_battery           : Battery current, in 10*milliamperes (1 = 10 milliampere), -1: autopilot does not measure the current (int16_t)
                battery_remaining         : Remaining battery energy: (0%: 0, 100%: 100), -1: autopilot estimate the remaining battery (int8_t)
                drop_rate_comm            : Communication drops in percent, (0%: 0, 100%: 10'000), (UART, I2C, SPI, CAN), dropped packets on all links (packets that were corrupted on reception on the MAV) (uint16_t)
                errors_comm               : Communication errors (UART, I2C, SPI, CAN), dropped packets on all links (packets that were corrupted on reception on the MAV) (uint16_t)
                errors_count1             : Autopilot-specific errors (uint16_t)
                errors_count2             : Autopilot-specific errors (uint16_t)
                errors_count3             : Autopilot-specific errors (uint16_t)
                errors_count4             : Autopilot-specific errors (uint16_t)

                '''
                return MAVLink_sys_status_message(onboard_control_sensors_present, onboard_control_sensors_enabled, onboard_control_sensors_health, load, voltage_battery, current_battery, battery_remaining, drop_rate_comm, errors_comm, errors_count1, errors_count2, errors_count3, errors_count4)

        def sys_status_send(self, onboard_control_sensors_present, onboard_control_sensors_enabled, onboard_control_sensors_health, load, voltage_battery, current_battery, battery_remaining, drop_rate_comm, errors_comm, errors_count1, errors_count2, errors_count3, errors_count4):
                '''
                The general system state. If the system is following the MAVLink
                standard, the system state is mainly defined by three
                orthogonal states/modes: The system mode, which is
                either LOCKED (motors shut down and locked), MANUAL
                (system under RC control), GUIDED (system with
                autonomous position control, position setpoint
                controlled manually) or AUTO (system guided by
                path/waypoint planner). The NAV_MODE defined the
                current flight state: LIFTOFF (often an open-loop
                maneuver), LANDING, WAYPOINTS or VECTOR. This
                represents the internal navigation state machine. The
                system status shows wether the system is currently
                active or not and if an emergency occured. During the
                CRITICAL and EMERGENCY states the MAV is still
                considered to be active, but should start emergency
                procedures autonomously. After a failure occured it
                should first move from active to critical to allow
                manual intervention and then move to emergency after a
                certain timeout.

                onboard_control_sensors_present        : Bitmask showing which onboard controllers and sensors are present. Value of 0: not present. Value of 1: present. Indices defined by ENUM MAV_SYS_STATUS_SENSOR (uint32_t)
                onboard_control_sensors_enabled        : Bitmask showing which onboard controllers and sensors are enabled:  Value of 0: not enabled. Value of 1: enabled. Indices defined by ENUM MAV_SYS_STATUS_SENSOR (uint32_t)
                onboard_control_sensors_health        : Bitmask showing which onboard controllers and sensors are operational or have an error:  Value of 0: not enabled. Value of 1: enabled. Indices defined by ENUM MAV_SYS_STATUS_SENSOR (uint32_t)
                load                      : Maximum usage in percent of the mainloop time, (0%: 0, 100%: 1000) should be always below 1000 (uint16_t)
                voltage_battery           : Battery voltage, in millivolts (1 = 1 millivolt) (uint16_t)
                current_battery           : Battery current, in 10*milliamperes (1 = 10 milliampere), -1: autopilot does not measure the current (int16_t)
                battery_remaining         : Remaining battery energy: (0%: 0, 100%: 100), -1: autopilot estimate the remaining battery (int8_t)
                drop_rate_comm            : Communication drops in percent, (0%: 0, 100%: 10'000), (UART, I2C, SPI, CAN), dropped packets on all links (packets that were corrupted on reception on the MAV) (uint16_t)
                errors_comm               : Communication errors (UART, I2C, SPI, CAN), dropped packets on all links (packets that were corrupted on reception on the MAV) (uint16_t)
                errors_count1             : Autopilot-specific errors (uint16_t)
                errors_count2             : Autopilot-specific errors (uint16_t)
                errors_count3             : Autopilot-specific errors (uint16_t)
                errors_count4             : Autopilot-specific errors (uint16_t)

                '''
                return self.send(self.sys_status_encode(onboard_control_sensors_present, onboard_control_sensors_enabled, onboard_control_sensors_health, load, voltage_battery, current_battery, battery_remaining, drop_rate_comm, errors_comm, errors_count1, errors_count2, errors_count3, errors_count4))

        def system_time_encode(self, time_unix_usec, time_boot_ms):
                '''
                The system time is the time of the master clock, typically the
                computer clock of the main onboard computer.

                time_unix_usec            : Timestamp of the master clock in microseconds since UNIX epoch. (uint64_t)
                time_boot_ms              : Timestamp of the component clock since boot time in milliseconds. (uint32_t)

                '''
                return MAVLink_system_time_message(time_unix_usec, time_boot_ms)

        def system_time_send(self, time_unix_usec, time_boot_ms):
                '''
                The system time is the time of the master clock, typically the
                computer clock of the main onboard computer.

                time_unix_usec            : Timestamp of the master clock in microseconds since UNIX epoch. (uint64_t)
                time_boot_ms              : Timestamp of the component clock since boot time in milliseconds. (uint32_t)

                '''
                return self.send(self.system_time_encode(time_unix_usec, time_boot_ms))

        def ping_encode(self, time_usec, seq, target_system, target_component):
                '''
                A ping message either requesting or responding to a ping. This allows
                to measure the system latencies, including serial
                port, radio modem and UDP connections.

                time_usec                 : Unix timestamp in microseconds or since system boot if smaller than MAVLink epoch (1.1.2009) (uint64_t)
                seq                       : PING sequence (uint32_t)
                target_system             : 0: request ping from all receiving systems, if greater than 0: message is a ping response and number is the system id of the requesting system (uint8_t)
                target_component          : 0: request ping from all receiving components, if greater than 0: message is a ping response and number is the system id of the requesting system (uint8_t)

                '''
                return MAVLink_ping_message(time_usec, seq, target_system, target_component)

        def ping_send(self, time_usec, seq, target_system, target_component):
                '''
                A ping message either requesting or responding to a ping. This allows
                to measure the system latencies, including serial
                port, radio modem and UDP connections.

                time_usec                 : Unix timestamp in microseconds or since system boot if smaller than MAVLink epoch (1.1.2009) (uint64_t)
                seq                       : PING sequence (uint32_t)
                target_system             : 0: request ping from all receiving systems, if greater than 0: message is a ping response and number is the system id of the requesting system (uint8_t)
                target_component          : 0: request ping from all receiving components, if greater than 0: message is a ping response and number is the system id of the requesting system (uint8_t)

                '''
                return self.send(self.ping_encode(time_usec, seq, target_system, target_component))

        def change_operator_control_encode(self, target_system, control_request, version, passkey):
                '''
                Request to control this MAV

                target_system             : System the GCS requests control for (uint8_t)
                control_request           : 0: request control of this MAV, 1: Release control of this MAV (uint8_t)
                version                   : 0: key as plaintext, 1-255: future, different hashing/encryption variants. The GCS should in general use the safest mode possible initially and then gradually move down the encryption level if it gets a NACK message indicating an encryption mismatch. (uint8_t)
                passkey                   : Password / Key, depending on version plaintext or encrypted. 25 or less characters, NULL terminated. The characters may involve A-Z, a-z, 0-9, and "!?,.-" (char)

                '''
                return MAVLink_change_operator_control_message(target_system, control_request, version, passkey)

        def change_operator_control_send(self, target_system, control_request, version, passkey):
                '''
                Request to control this MAV

                target_system             : System the GCS requests control for (uint8_t)
                control_request           : 0: request control of this MAV, 1: Release control of this MAV (uint8_t)
                version                   : 0: key as plaintext, 1-255: future, different hashing/encryption variants. The GCS should in general use the safest mode possible initially and then gradually move down the encryption level if it gets a NACK message indicating an encryption mismatch. (uint8_t)
                passkey                   : Password / Key, depending on version plaintext or encrypted. 25 or less characters, NULL terminated. The characters may involve A-Z, a-z, 0-9, and "!?,.-" (char)

                '''
                return self.send(self.change_operator_control_encode(target_system, control_request, version, passkey))

        def change_operator_control_ack_encode(self, gcs_system_id, control_request, ack):
                '''
                Accept / deny control of this MAV

                gcs_system_id             : ID of the GCS this message (uint8_t)
                control_request           : 0: request control of this MAV, 1: Release control of this MAV (uint8_t)
                ack                       : 0: ACK, 1: NACK: Wrong passkey, 2: NACK: Unsupported passkey encryption method, 3: NACK: Already under control (uint8_t)

                '''
                return MAVLink_change_operator_control_ack_message(gcs_system_id, control_request, ack)

        def change_operator_control_ack_send(self, gcs_system_id, control_request, ack):
                '''
                Accept / deny control of this MAV

                gcs_system_id             : ID of the GCS this message (uint8_t)
                control_request           : 0: request control of this MAV, 1: Release control of this MAV (uint8_t)
                ack                       : 0: ACK, 1: NACK: Wrong passkey, 2: NACK: Unsupported passkey encryption method, 3: NACK: Already under control (uint8_t)

                '''
                return self.send(self.change_operator_control_ack_encode(gcs_system_id, control_request, ack))

        def auth_key_encode(self, key):
                '''
                Emit an encrypted signature / key identifying this system. PLEASE
                NOTE: This protocol has been kept simple, so
                transmitting the key requires an encrypted channel for
                true safety.

                key                       : key (char)

                '''
                return MAVLink_auth_key_message(key)

        def auth_key_send(self, key):
                '''
                Emit an encrypted signature / key identifying this system. PLEASE
                NOTE: This protocol has been kept simple, so
                transmitting the key requires an encrypted channel for
                true safety.

                key                       : key (char)

                '''
                return self.send(self.auth_key_encode(key))

        def set_mode_encode(self, target_system, base_mode, custom_mode):
                '''
                Set the system mode, as defined by enum MAV_MODE. There is no target
                component id as the mode is by definition for the
                overall aircraft, not only for one component.

                target_system             : The system setting the mode (uint8_t)
                base_mode                 : The new base mode (uint8_t)
                custom_mode               : The new autopilot-specific mode. This field can be ignored by an autopilot. (uint32_t)

                '''
                return MAVLink_set_mode_message(target_system, base_mode, custom_mode)

        def set_mode_send(self, target_system, base_mode, custom_mode):
                '''
                Set the system mode, as defined by enum MAV_MODE. There is no target
                component id as the mode is by definition for the
                overall aircraft, not only for one component.

                target_system             : The system setting the mode (uint8_t)
                base_mode                 : The new base mode (uint8_t)
                custom_mode               : The new autopilot-specific mode. This field can be ignored by an autopilot. (uint32_t)

                '''
                return self.send(self.set_mode_encode(target_system, base_mode, custom_mode))

        def param_request_read_encode(self, target_system, target_component, param_id, param_index):
                '''
                Request to read the onboard parameter with the param_id string id.
                Onboard parameters are stored as key[const char*] ->
                value[float]. This allows to send a parameter to any
                other component (such as the GCS) without the need of
                previous knowledge of possible parameter names. Thus
                the same GCS can store different parameters for
                different autopilots. See also
                http://qgroundcontrol.org/parameter_interface for a
                full documentation of QGroundControl and IMU code.

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                param_id                  : Onboard parameter id, terminated by NULL if the length is less than 16 human-readable chars and WITHOUT null termination (NULL) byte if the length is exactly 16 chars - applications have to provide 16+1 bytes storage if the ID is stored as string (char)
                param_index               : Parameter index. Send -1 to use the param ID field as identifier (else the param id will be ignored) (int16_t)

                '''
                return MAVLink_param_request_read_message(target_system, target_component, param_id, param_index)

        def param_request_read_send(self, target_system, target_component, param_id, param_index):
                '''
                Request to read the onboard parameter with the param_id string id.
                Onboard parameters are stored as key[const char*] ->
                value[float]. This allows to send a parameter to any
                other component (such as the GCS) without the need of
                previous knowledge of possible parameter names. Thus
                the same GCS can store different parameters for
                different autopilots. See also
                http://qgroundcontrol.org/parameter_interface for a
                full documentation of QGroundControl and IMU code.

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                param_id                  : Onboard parameter id, terminated by NULL if the length is less than 16 human-readable chars and WITHOUT null termination (NULL) byte if the length is exactly 16 chars - applications have to provide 16+1 bytes storage if the ID is stored as string (char)
                param_index               : Parameter index. Send -1 to use the param ID field as identifier (else the param id will be ignored) (int16_t)

                '''
                return self.send(self.param_request_read_encode(target_system, target_component, param_id, param_index))

        def param_request_list_encode(self, target_system, target_component):
                '''
                Request all parameters of this component. After his request, all
                parameters are emitted.

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)

                '''
                return MAVLink_param_request_list_message(target_system, target_component)

        def param_request_list_send(self, target_system, target_component):
                '''
                Request all parameters of this component. After his request, all
                parameters are emitted.

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)

                '''
                return self.send(self.param_request_list_encode(target_system, target_component))

        def param_value_encode(self, param_id, param_value, param_type, param_count, param_index):
                '''
                Emit the value of a onboard parameter. The inclusion of param_count
                and param_index in the message allows the recipient to
                keep track of received parameters and allows him to
                re-request missing parameters after a loss or timeout.

                param_id                  : Onboard parameter id, terminated by NULL if the length is less than 16 human-readable chars and WITHOUT null termination (NULL) byte if the length is exactly 16 chars - applications have to provide 16+1 bytes storage if the ID is stored as string (char)
                param_value               : Onboard parameter value (float)
                param_type                : Onboard parameter type: see the MAV_PARAM_TYPE enum for supported data types. (uint8_t)
                param_count               : Total number of onboard parameters (uint16_t)
                param_index               : Index of this onboard parameter (uint16_t)

                '''
                return MAVLink_param_value_message(param_id, param_value, param_type, param_count, param_index)

        def param_value_send(self, param_id, param_value, param_type, param_count, param_index):
                '''
                Emit the value of a onboard parameter. The inclusion of param_count
                and param_index in the message allows the recipient to
                keep track of received parameters and allows him to
                re-request missing parameters after a loss or timeout.

                param_id                  : Onboard parameter id, terminated by NULL if the length is less than 16 human-readable chars and WITHOUT null termination (NULL) byte if the length is exactly 16 chars - applications have to provide 16+1 bytes storage if the ID is stored as string (char)
                param_value               : Onboard parameter value (float)
                param_type                : Onboard parameter type: see the MAV_PARAM_TYPE enum for supported data types. (uint8_t)
                param_count               : Total number of onboard parameters (uint16_t)
                param_index               : Index of this onboard parameter (uint16_t)

                '''
                return self.send(self.param_value_encode(param_id, param_value, param_type, param_count, param_index))

        def param_set_encode(self, target_system, target_component, param_id, param_value, param_type):
                '''
                Set a parameter value TEMPORARILY to RAM. It will be reset to default
                on system reboot. Send the ACTION
                MAV_ACTION_STORAGE_WRITE to PERMANENTLY write the RAM
                contents to EEPROM. IMPORTANT: The receiving component
                should acknowledge the new parameter value by sending
                a param_value message to all communication partners.
                This will also ensure that multiple GCS all have an
                up-to-date list of all parameters. If the sending GCS
                did not receive a PARAM_VALUE message within its
                timeout time, it should re-send the PARAM_SET message.

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                param_id                  : Onboard parameter id, terminated by NULL if the length is less than 16 human-readable chars and WITHOUT null termination (NULL) byte if the length is exactly 16 chars - applications have to provide 16+1 bytes storage if the ID is stored as string (char)
                param_value               : Onboard parameter value (float)
                param_type                : Onboard parameter type: see the MAV_PARAM_TYPE enum for supported data types. (uint8_t)

                '''
                return MAVLink_param_set_message(target_system, target_component, param_id, param_value, param_type)

        def param_set_send(self, target_system, target_component, param_id, param_value, param_type):
                '''
                Set a parameter value TEMPORARILY to RAM. It will be reset to default
                on system reboot. Send the ACTION
                MAV_ACTION_STORAGE_WRITE to PERMANENTLY write the RAM
                contents to EEPROM. IMPORTANT: The receiving component
                should acknowledge the new parameter value by sending
                a param_value message to all communication partners.
                This will also ensure that multiple GCS all have an
                up-to-date list of all parameters. If the sending GCS
                did not receive a PARAM_VALUE message within its
                timeout time, it should re-send the PARAM_SET message.

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                param_id                  : Onboard parameter id, terminated by NULL if the length is less than 16 human-readable chars and WITHOUT null termination (NULL) byte if the length is exactly 16 chars - applications have to provide 16+1 bytes storage if the ID is stored as string (char)
                param_value               : Onboard parameter value (float)
                param_type                : Onboard parameter type: see the MAV_PARAM_TYPE enum for supported data types. (uint8_t)

                '''
                return self.send(self.param_set_encode(target_system, target_component, param_id, param_value, param_type))

        def gps_raw_int_encode(self, time_usec, fix_type, lat, lon, alt, eph, epv, vel, cog, satellites_visible):
                '''
                The global position, as returned by the Global Positioning System
                (GPS). This is                 NOT the global position
                estimate of the system, but rather a RAW sensor value.
                See message GLOBAL_POSITION for the global position
                estimate. Coordinate frame is right-handed, Z-axis up
                (GPS frame).

                time_usec                 : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
                fix_type                  : 0-1: no fix, 2: 2D fix, 3: 3D fix, 4: DGPS, 5: RTK. Some applications will not use the value of this field unless it is at least two, so always correctly fill in the fix. (uint8_t)
                lat                       : Latitude (WGS84), in degrees * 1E7 (int32_t)
                lon                       : Longitude (WGS84), in degrees * 1E7 (int32_t)
                alt                       : Altitude (AMSL, NOT WGS84), in meters * 1000 (positive for up). Note that virtually all GPS modules provide the AMSL altitude in addition to the WGS84 altitude. (int32_t)
                eph                       : GPS HDOP horizontal dilution of position in cm (m*100). If unknown, set to: UINT16_MAX (uint16_t)
                epv                       : GPS VDOP vertical dilution of position in cm (m*100). If unknown, set to: UINT16_MAX (uint16_t)
                vel                       : GPS ground speed (m/s * 100). If unknown, set to: UINT16_MAX (uint16_t)
                cog                       : Course over ground (NOT heading, but direction of movement) in degrees * 100, 0.0..359.99 degrees. If unknown, set to: UINT16_MAX (uint16_t)
                satellites_visible        : Number of satellites visible. If unknown, set to 255 (uint8_t)

                '''
                return MAVLink_gps_raw_int_message(time_usec, fix_type, lat, lon, alt, eph, epv, vel, cog, satellites_visible)

        def gps_raw_int_send(self, time_usec, fix_type, lat, lon, alt, eph, epv, vel, cog, satellites_visible):
                '''
                The global position, as returned by the Global Positioning System
                (GPS). This is                 NOT the global position
                estimate of the system, but rather a RAW sensor value.
                See message GLOBAL_POSITION for the global position
                estimate. Coordinate frame is right-handed, Z-axis up
                (GPS frame).

                time_usec                 : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
                fix_type                  : 0-1: no fix, 2: 2D fix, 3: 3D fix, 4: DGPS, 5: RTK. Some applications will not use the value of this field unless it is at least two, so always correctly fill in the fix. (uint8_t)
                lat                       : Latitude (WGS84), in degrees * 1E7 (int32_t)
                lon                       : Longitude (WGS84), in degrees * 1E7 (int32_t)
                alt                       : Altitude (AMSL, NOT WGS84), in meters * 1000 (positive for up). Note that virtually all GPS modules provide the AMSL altitude in addition to the WGS84 altitude. (int32_t)
                eph                       : GPS HDOP horizontal dilution of position in cm (m*100). If unknown, set to: UINT16_MAX (uint16_t)
                epv                       : GPS VDOP vertical dilution of position in cm (m*100). If unknown, set to: UINT16_MAX (uint16_t)
                vel                       : GPS ground speed (m/s * 100). If unknown, set to: UINT16_MAX (uint16_t)
                cog                       : Course over ground (NOT heading, but direction of movement) in degrees * 100, 0.0..359.99 degrees. If unknown, set to: UINT16_MAX (uint16_t)
                satellites_visible        : Number of satellites visible. If unknown, set to 255 (uint8_t)

                '''
                return self.send(self.gps_raw_int_encode(time_usec, fix_type, lat, lon, alt, eph, epv, vel, cog, satellites_visible))

        def gps_status_encode(self, satellites_visible, satellite_prn, satellite_used, satellite_elevation, satellite_azimuth, satellite_snr):
                '''
                The positioning status, as reported by GPS. This message is intended
                to display status information about each satellite
                visible to the receiver. See message GLOBAL_POSITION
                for the global position estimate. This message can
                contain information for up to 20 satellites.

                satellites_visible        : Number of satellites visible (uint8_t)
                satellite_prn             : Global satellite ID (uint8_t)
                satellite_used            : 0: Satellite not used, 1: used for localization (uint8_t)
                satellite_elevation        : Elevation (0: right on top of receiver, 90: on the horizon) of satellite (uint8_t)
                satellite_azimuth         : Direction of satellite, 0: 0 deg, 255: 360 deg. (uint8_t)
                satellite_snr             : Signal to noise ratio of satellite (uint8_t)

                '''
                return MAVLink_gps_status_message(satellites_visible, satellite_prn, satellite_used, satellite_elevation, satellite_azimuth, satellite_snr)

        def gps_status_send(self, satellites_visible, satellite_prn, satellite_used, satellite_elevation, satellite_azimuth, satellite_snr):
                '''
                The positioning status, as reported by GPS. This message is intended
                to display status information about each satellite
                visible to the receiver. See message GLOBAL_POSITION
                for the global position estimate. This message can
                contain information for up to 20 satellites.

                satellites_visible        : Number of satellites visible (uint8_t)
                satellite_prn             : Global satellite ID (uint8_t)
                satellite_used            : 0: Satellite not used, 1: used for localization (uint8_t)
                satellite_elevation        : Elevation (0: right on top of receiver, 90: on the horizon) of satellite (uint8_t)
                satellite_azimuth         : Direction of satellite, 0: 0 deg, 255: 360 deg. (uint8_t)
                satellite_snr             : Signal to noise ratio of satellite (uint8_t)

                '''
                return self.send(self.gps_status_encode(satellites_visible, satellite_prn, satellite_used, satellite_elevation, satellite_azimuth, satellite_snr))

        def scaled_imu_encode(self, time_boot_ms, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag):
                '''
                The RAW IMU readings for the usual 9DOF sensor setup. This message
                should contain the scaled values to the described
                units

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                xacc                      : X acceleration (mg) (int16_t)
                yacc                      : Y acceleration (mg) (int16_t)
                zacc                      : Z acceleration (mg) (int16_t)
                xgyro                     : Angular speed around X axis (millirad /sec) (int16_t)
                ygyro                     : Angular speed around Y axis (millirad /sec) (int16_t)
                zgyro                     : Angular speed around Z axis (millirad /sec) (int16_t)
                xmag                      : X Magnetic field (milli tesla) (int16_t)
                ymag                      : Y Magnetic field (milli tesla) (int16_t)
                zmag                      : Z Magnetic field (milli tesla) (int16_t)

                '''
                return MAVLink_scaled_imu_message(time_boot_ms, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag)

        def scaled_imu_send(self, time_boot_ms, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag):
                '''
                The RAW IMU readings for the usual 9DOF sensor setup. This message
                should contain the scaled values to the described
                units

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                xacc                      : X acceleration (mg) (int16_t)
                yacc                      : Y acceleration (mg) (int16_t)
                zacc                      : Z acceleration (mg) (int16_t)
                xgyro                     : Angular speed around X axis (millirad /sec) (int16_t)
                ygyro                     : Angular speed around Y axis (millirad /sec) (int16_t)
                zgyro                     : Angular speed around Z axis (millirad /sec) (int16_t)
                xmag                      : X Magnetic field (milli tesla) (int16_t)
                ymag                      : Y Magnetic field (milli tesla) (int16_t)
                zmag                      : Z Magnetic field (milli tesla) (int16_t)

                '''
                return self.send(self.scaled_imu_encode(time_boot_ms, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag))

        def raw_imu_encode(self, time_usec, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag):
                '''
                The RAW IMU readings for the usual 9DOF sensor setup. This message
                should always contain the true raw values without any
                scaling to allow data capture and system debugging.

                time_usec                 : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
                xacc                      : X acceleration (raw) (int16_t)
                yacc                      : Y acceleration (raw) (int16_t)
                zacc                      : Z acceleration (raw) (int16_t)
                xgyro                     : Angular speed around X axis (raw) (int16_t)
                ygyro                     : Angular speed around Y axis (raw) (int16_t)
                zgyro                     : Angular speed around Z axis (raw) (int16_t)
                xmag                      : X Magnetic field (raw) (int16_t)
                ymag                      : Y Magnetic field (raw) (int16_t)
                zmag                      : Z Magnetic field (raw) (int16_t)

                '''
                return MAVLink_raw_imu_message(time_usec, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag)

        def raw_imu_send(self, time_usec, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag):
                '''
                The RAW IMU readings for the usual 9DOF sensor setup. This message
                should always contain the true raw values without any
                scaling to allow data capture and system debugging.

                time_usec                 : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
                xacc                      : X acceleration (raw) (int16_t)
                yacc                      : Y acceleration (raw) (int16_t)
                zacc                      : Z acceleration (raw) (int16_t)
                xgyro                     : Angular speed around X axis (raw) (int16_t)
                ygyro                     : Angular speed around Y axis (raw) (int16_t)
                zgyro                     : Angular speed around Z axis (raw) (int16_t)
                xmag                      : X Magnetic field (raw) (int16_t)
                ymag                      : Y Magnetic field (raw) (int16_t)
                zmag                      : Z Magnetic field (raw) (int16_t)

                '''
                return self.send(self.raw_imu_encode(time_usec, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag))

        def raw_pressure_encode(self, time_usec, press_abs, press_diff1, press_diff2, temperature):
                '''
                The RAW pressure readings for the typical setup of one absolute
                pressure and one differential pressure sensor. The
                sensor values should be the raw, UNSCALED ADC values.

                time_usec                 : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
                press_abs                 : Absolute pressure (raw) (int16_t)
                press_diff1               : Differential pressure 1 (raw) (int16_t)
                press_diff2               : Differential pressure 2 (raw) (int16_t)
                temperature               : Raw Temperature measurement (raw) (int16_t)

                '''
                return MAVLink_raw_pressure_message(time_usec, press_abs, press_diff1, press_diff2, temperature)

        def raw_pressure_send(self, time_usec, press_abs, press_diff1, press_diff2, temperature):
                '''
                The RAW pressure readings for the typical setup of one absolute
                pressure and one differential pressure sensor. The
                sensor values should be the raw, UNSCALED ADC values.

                time_usec                 : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
                press_abs                 : Absolute pressure (raw) (int16_t)
                press_diff1               : Differential pressure 1 (raw) (int16_t)
                press_diff2               : Differential pressure 2 (raw) (int16_t)
                temperature               : Raw Temperature measurement (raw) (int16_t)

                '''
                return self.send(self.raw_pressure_encode(time_usec, press_abs, press_diff1, press_diff2, temperature))

        def scaled_pressure_encode(self, time_boot_ms, press_abs, press_diff, temperature):
                '''
                The pressure readings for the typical setup of one absolute and
                differential pressure sensor. The units are as
                specified in each field.

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                press_abs                 : Absolute pressure (hectopascal) (float)
                press_diff                : Differential pressure 1 (hectopascal) (float)
                temperature               : Temperature measurement (0.01 degrees celsius) (int16_t)

                '''
                return MAVLink_scaled_pressure_message(time_boot_ms, press_abs, press_diff, temperature)

        def scaled_pressure_send(self, time_boot_ms, press_abs, press_diff, temperature):
                '''
                The pressure readings for the typical setup of one absolute and
                differential pressure sensor. The units are as
                specified in each field.

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                press_abs                 : Absolute pressure (hectopascal) (float)
                press_diff                : Differential pressure 1 (hectopascal) (float)
                temperature               : Temperature measurement (0.01 degrees celsius) (int16_t)

                '''
                return self.send(self.scaled_pressure_encode(time_boot_ms, press_abs, press_diff, temperature))

        def attitude_encode(self, time_boot_ms, roll, pitch, yaw, rollspeed, pitchspeed, yawspeed):
                '''
                The attitude in the aeronautical frame (right-handed, Z-down, X-front,
                Y-right).

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                roll                      : Roll angle (rad, -pi..+pi) (float)
                pitch                     : Pitch angle (rad, -pi..+pi) (float)
                yaw                       : Yaw angle (rad, -pi..+pi) (float)
                rollspeed                 : Roll angular speed (rad/s) (float)
                pitchspeed                : Pitch angular speed (rad/s) (float)
                yawspeed                  : Yaw angular speed (rad/s) (float)

                '''
                return MAVLink_attitude_message(time_boot_ms, roll, pitch, yaw, rollspeed, pitchspeed, yawspeed)

        def attitude_send(self, time_boot_ms, roll, pitch, yaw, rollspeed, pitchspeed, yawspeed):
                '''
                The attitude in the aeronautical frame (right-handed, Z-down, X-front,
                Y-right).

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                roll                      : Roll angle (rad, -pi..+pi) (float)
                pitch                     : Pitch angle (rad, -pi..+pi) (float)
                yaw                       : Yaw angle (rad, -pi..+pi) (float)
                rollspeed                 : Roll angular speed (rad/s) (float)
                pitchspeed                : Pitch angular speed (rad/s) (float)
                yawspeed                  : Yaw angular speed (rad/s) (float)

                '''
                return self.send(self.attitude_encode(time_boot_ms, roll, pitch, yaw, rollspeed, pitchspeed, yawspeed))

        def attitude_quaternion_encode(self, time_boot_ms, q1, q2, q3, q4, rollspeed, pitchspeed, yawspeed):
                '''
                The attitude in the aeronautical frame (right-handed, Z-down, X-front,
                Y-right), expressed as quaternion. Quaternion order is
                w, x, y, z and a zero rotation would be expressed as
                (1 0 0 0).

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                q1                        : Quaternion component 1, w (1 in null-rotation) (float)
                q2                        : Quaternion component 2, x (0 in null-rotation) (float)
                q3                        : Quaternion component 3, y (0 in null-rotation) (float)
                q4                        : Quaternion component 4, z (0 in null-rotation) (float)
                rollspeed                 : Roll angular speed (rad/s) (float)
                pitchspeed                : Pitch angular speed (rad/s) (float)
                yawspeed                  : Yaw angular speed (rad/s) (float)

                '''
                return MAVLink_attitude_quaternion_message(time_boot_ms, q1, q2, q3, q4, rollspeed, pitchspeed, yawspeed)

        def attitude_quaternion_send(self, time_boot_ms, q1, q2, q3, q4, rollspeed, pitchspeed, yawspeed):
                '''
                The attitude in the aeronautical frame (right-handed, Z-down, X-front,
                Y-right), expressed as quaternion. Quaternion order is
                w, x, y, z and a zero rotation would be expressed as
                (1 0 0 0).

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                q1                        : Quaternion component 1, w (1 in null-rotation) (float)
                q2                        : Quaternion component 2, x (0 in null-rotation) (float)
                q3                        : Quaternion component 3, y (0 in null-rotation) (float)
                q4                        : Quaternion component 4, z (0 in null-rotation) (float)
                rollspeed                 : Roll angular speed (rad/s) (float)
                pitchspeed                : Pitch angular speed (rad/s) (float)
                yawspeed                  : Yaw angular speed (rad/s) (float)

                '''
                return self.send(self.attitude_quaternion_encode(time_boot_ms, q1, q2, q3, q4, rollspeed, pitchspeed, yawspeed))

        def local_position_ned_encode(self, time_boot_ms, x, y, z, vx, vy, vz):
                '''
                The filtered local position (e.g. fused computer vision and
                accelerometers). Coordinate frame is right-handed,
                Z-axis down (aeronautical frame, NED / north-east-down
                convention)

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                x                         : X Position (float)
                y                         : Y Position (float)
                z                         : Z Position (float)
                vx                        : X Speed (float)
                vy                        : Y Speed (float)
                vz                        : Z Speed (float)

                '''
                return MAVLink_local_position_ned_message(time_boot_ms, x, y, z, vx, vy, vz)

        def local_position_ned_send(self, time_boot_ms, x, y, z, vx, vy, vz):
                '''
                The filtered local position (e.g. fused computer vision and
                accelerometers). Coordinate frame is right-handed,
                Z-axis down (aeronautical frame, NED / north-east-down
                convention)

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                x                         : X Position (float)
                y                         : Y Position (float)
                z                         : Z Position (float)
                vx                        : X Speed (float)
                vy                        : Y Speed (float)
                vz                        : Z Speed (float)

                '''
                return self.send(self.local_position_ned_encode(time_boot_ms, x, y, z, vx, vy, vz))

        def global_position_int_encode(self, time_boot_ms, lat, lon, alt, relative_alt, vx, vy, vz, hdg):
                '''
                The filtered global position (e.g. fused GPS and accelerometers). The
                position is in GPS-frame (right-handed, Z-up). It
                is designed as scaled integer message since the
                resolution of float is not sufficient.

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                lat                       : Latitude, expressed as * 1E7 (int32_t)
                lon                       : Longitude, expressed as * 1E7 (int32_t)
                alt                       : Altitude in meters, expressed as * 1000 (millimeters), AMSL (not WGS84 - note that virtually all GPS modules provide the AMSL as well) (int32_t)
                relative_alt              : Altitude above ground in meters, expressed as * 1000 (millimeters) (int32_t)
                vx                        : Ground X Speed (Latitude), expressed as m/s * 100 (int16_t)
                vy                        : Ground Y Speed (Longitude), expressed as m/s * 100 (int16_t)
                vz                        : Ground Z Speed (Altitude), expressed as m/s * 100 (int16_t)
                hdg                       : Compass heading in degrees * 100, 0.0..359.99 degrees. If unknown, set to: UINT16_MAX (uint16_t)

                '''
                return MAVLink_global_position_int_message(time_boot_ms, lat, lon, alt, relative_alt, vx, vy, vz, hdg)

        def global_position_int_send(self, time_boot_ms, lat, lon, alt, relative_alt, vx, vy, vz, hdg):
                '''
                The filtered global position (e.g. fused GPS and accelerometers). The
                position is in GPS-frame (right-handed, Z-up). It
                is designed as scaled integer message since the
                resolution of float is not sufficient.

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                lat                       : Latitude, expressed as * 1E7 (int32_t)
                lon                       : Longitude, expressed as * 1E7 (int32_t)
                alt                       : Altitude in meters, expressed as * 1000 (millimeters), AMSL (not WGS84 - note that virtually all GPS modules provide the AMSL as well) (int32_t)
                relative_alt              : Altitude above ground in meters, expressed as * 1000 (millimeters) (int32_t)
                vx                        : Ground X Speed (Latitude), expressed as m/s * 100 (int16_t)
                vy                        : Ground Y Speed (Longitude), expressed as m/s * 100 (int16_t)
                vz                        : Ground Z Speed (Altitude), expressed as m/s * 100 (int16_t)
                hdg                       : Compass heading in degrees * 100, 0.0..359.99 degrees. If unknown, set to: UINT16_MAX (uint16_t)

                '''
                return self.send(self.global_position_int_encode(time_boot_ms, lat, lon, alt, relative_alt, vx, vy, vz, hdg))

        def rc_channels_scaled_encode(self, time_boot_ms, port, chan1_scaled, chan2_scaled, chan3_scaled, chan4_scaled, chan5_scaled, chan6_scaled, chan7_scaled, chan8_scaled, rssi):
                '''
                The scaled values of the RC channels received. (-100%) -10000, (0%) 0,
                (100%) 10000. Channels that are inactive should be set
                to UINT16_MAX.

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                port                      : Servo output port (set of 8 outputs = 1 port). Most MAVs will just use one, but this allows for more than 8 servos. (uint8_t)
                chan1_scaled              : RC channel 1 value scaled, (-100%) -10000, (0%) 0, (100%) 10000, (invalid) INT16_MAX. (int16_t)
                chan2_scaled              : RC channel 2 value scaled, (-100%) -10000, (0%) 0, (100%) 10000, (invalid) INT16_MAX. (int16_t)
                chan3_scaled              : RC channel 3 value scaled, (-100%) -10000, (0%) 0, (100%) 10000, (invalid) INT16_MAX. (int16_t)
                chan4_scaled              : RC channel 4 value scaled, (-100%) -10000, (0%) 0, (100%) 10000, (invalid) INT16_MAX. (int16_t)
                chan5_scaled              : RC channel 5 value scaled, (-100%) -10000, (0%) 0, (100%) 10000, (invalid) INT16_MAX. (int16_t)
                chan6_scaled              : RC channel 6 value scaled, (-100%) -10000, (0%) 0, (100%) 10000, (invalid) INT16_MAX. (int16_t)
                chan7_scaled              : RC channel 7 value scaled, (-100%) -10000, (0%) 0, (100%) 10000, (invalid) INT16_MAX. (int16_t)
                chan8_scaled              : RC channel 8 value scaled, (-100%) -10000, (0%) 0, (100%) 10000, (invalid) INT16_MAX. (int16_t)
                rssi                      : Receive signal strength indicator, 0: 0%, 100: 100%, 255: invalid/unknown. (uint8_t)

                '''
                return MAVLink_rc_channels_scaled_message(time_boot_ms, port, chan1_scaled, chan2_scaled, chan3_scaled, chan4_scaled, chan5_scaled, chan6_scaled, chan7_scaled, chan8_scaled, rssi)

        def rc_channels_scaled_send(self, time_boot_ms, port, chan1_scaled, chan2_scaled, chan3_scaled, chan4_scaled, chan5_scaled, chan6_scaled, chan7_scaled, chan8_scaled, rssi):
                '''
                The scaled values of the RC channels received. (-100%) -10000, (0%) 0,
                (100%) 10000. Channels that are inactive should be set
                to UINT16_MAX.

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                port                      : Servo output port (set of 8 outputs = 1 port). Most MAVs will just use one, but this allows for more than 8 servos. (uint8_t)
                chan1_scaled              : RC channel 1 value scaled, (-100%) -10000, (0%) 0, (100%) 10000, (invalid) INT16_MAX. (int16_t)
                chan2_scaled              : RC channel 2 value scaled, (-100%) -10000, (0%) 0, (100%) 10000, (invalid) INT16_MAX. (int16_t)
                chan3_scaled              : RC channel 3 value scaled, (-100%) -10000, (0%) 0, (100%) 10000, (invalid) INT16_MAX. (int16_t)
                chan4_scaled              : RC channel 4 value scaled, (-100%) -10000, (0%) 0, (100%) 10000, (invalid) INT16_MAX. (int16_t)
                chan5_scaled              : RC channel 5 value scaled, (-100%) -10000, (0%) 0, (100%) 10000, (invalid) INT16_MAX. (int16_t)
                chan6_scaled              : RC channel 6 value scaled, (-100%) -10000, (0%) 0, (100%) 10000, (invalid) INT16_MAX. (int16_t)
                chan7_scaled              : RC channel 7 value scaled, (-100%) -10000, (0%) 0, (100%) 10000, (invalid) INT16_MAX. (int16_t)
                chan8_scaled              : RC channel 8 value scaled, (-100%) -10000, (0%) 0, (100%) 10000, (invalid) INT16_MAX. (int16_t)
                rssi                      : Receive signal strength indicator, 0: 0%, 100: 100%, 255: invalid/unknown. (uint8_t)

                '''
                return self.send(self.rc_channels_scaled_encode(time_boot_ms, port, chan1_scaled, chan2_scaled, chan3_scaled, chan4_scaled, chan5_scaled, chan6_scaled, chan7_scaled, chan8_scaled, rssi))

        def rc_channels_raw_encode(self, time_boot_ms, port, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw, rssi):
                '''
                The RAW values of the RC channels received. The standard PPM
                modulation is as follows: 1000 microseconds: 0%, 2000
                microseconds: 100%. Individual receivers/transmitters
                might violate this specification.

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                port                      : Servo output port (set of 8 outputs = 1 port). Most MAVs will just use one, but this allows for more than 8 servos. (uint8_t)
                chan1_raw                 : RC channel 1 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan2_raw                 : RC channel 2 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan3_raw                 : RC channel 3 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan4_raw                 : RC channel 4 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan5_raw                 : RC channel 5 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan6_raw                 : RC channel 6 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan7_raw                 : RC channel 7 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan8_raw                 : RC channel 8 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                rssi                      : Receive signal strength indicator, 0: 0%, 100: 100%, 255: invalid/unknown. (uint8_t)

                '''
                return MAVLink_rc_channels_raw_message(time_boot_ms, port, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw, rssi)

        def rc_channels_raw_send(self, time_boot_ms, port, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw, rssi):
                '''
                The RAW values of the RC channels received. The standard PPM
                modulation is as follows: 1000 microseconds: 0%, 2000
                microseconds: 100%. Individual receivers/transmitters
                might violate this specification.

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                port                      : Servo output port (set of 8 outputs = 1 port). Most MAVs will just use one, but this allows for more than 8 servos. (uint8_t)
                chan1_raw                 : RC channel 1 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan2_raw                 : RC channel 2 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan3_raw                 : RC channel 3 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan4_raw                 : RC channel 4 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan5_raw                 : RC channel 5 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan6_raw                 : RC channel 6 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan7_raw                 : RC channel 7 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan8_raw                 : RC channel 8 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                rssi                      : Receive signal strength indicator, 0: 0%, 100: 100%, 255: invalid/unknown. (uint8_t)

                '''
                return self.send(self.rc_channels_raw_encode(time_boot_ms, port, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw, rssi))

        def servo_output_raw_encode(self, time_usec, port, servo1_raw, servo2_raw, servo3_raw, servo4_raw, servo5_raw, servo6_raw, servo7_raw, servo8_raw):
                '''
                The RAW values of the servo outputs (for RC input from the remote, use
                the RC_CHANNELS messages). The standard PPM modulation
                is as follows: 1000 microseconds: 0%, 2000
                microseconds: 100%.

                time_usec                 : Timestamp (microseconds since system boot) (uint32_t)
                port                      : Servo output port (set of 8 outputs = 1 port). Most MAVs will just use one, but this allows to encode more than 8 servos. (uint8_t)
                servo1_raw                : Servo output 1 value, in microseconds (uint16_t)
                servo2_raw                : Servo output 2 value, in microseconds (uint16_t)
                servo3_raw                : Servo output 3 value, in microseconds (uint16_t)
                servo4_raw                : Servo output 4 value, in microseconds (uint16_t)
                servo5_raw                : Servo output 5 value, in microseconds (uint16_t)
                servo6_raw                : Servo output 6 value, in microseconds (uint16_t)
                servo7_raw                : Servo output 7 value, in microseconds (uint16_t)
                servo8_raw                : Servo output 8 value, in microseconds (uint16_t)

                '''
                return MAVLink_servo_output_raw_message(time_usec, port, servo1_raw, servo2_raw, servo3_raw, servo4_raw, servo5_raw, servo6_raw, servo7_raw, servo8_raw)

        def servo_output_raw_send(self, time_usec, port, servo1_raw, servo2_raw, servo3_raw, servo4_raw, servo5_raw, servo6_raw, servo7_raw, servo8_raw):
                '''
                The RAW values of the servo outputs (for RC input from the remote, use
                the RC_CHANNELS messages). The standard PPM modulation
                is as follows: 1000 microseconds: 0%, 2000
                microseconds: 100%.

                time_usec                 : Timestamp (microseconds since system boot) (uint32_t)
                port                      : Servo output port (set of 8 outputs = 1 port). Most MAVs will just use one, but this allows to encode more than 8 servos. (uint8_t)
                servo1_raw                : Servo output 1 value, in microseconds (uint16_t)
                servo2_raw                : Servo output 2 value, in microseconds (uint16_t)
                servo3_raw                : Servo output 3 value, in microseconds (uint16_t)
                servo4_raw                : Servo output 4 value, in microseconds (uint16_t)
                servo5_raw                : Servo output 5 value, in microseconds (uint16_t)
                servo6_raw                : Servo output 6 value, in microseconds (uint16_t)
                servo7_raw                : Servo output 7 value, in microseconds (uint16_t)
                servo8_raw                : Servo output 8 value, in microseconds (uint16_t)

                '''
                return self.send(self.servo_output_raw_encode(time_usec, port, servo1_raw, servo2_raw, servo3_raw, servo4_raw, servo5_raw, servo6_raw, servo7_raw, servo8_raw))

        def mission_request_partial_list_encode(self, target_system, target_component, start_index, end_index):
                '''
                Request a partial list of mission items from the system/component.
                http://qgroundcontrol.org/mavlink/waypoint_protocol.
                If start and end index are the same, just send one
                waypoint.

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                start_index               : Start index, 0 by default (int16_t)
                end_index                 : End index, -1 by default (-1: send list to end). Else a valid index of the list (int16_t)

                '''
                return MAVLink_mission_request_partial_list_message(target_system, target_component, start_index, end_index)

        def mission_request_partial_list_send(self, target_system, target_component, start_index, end_index):
                '''
                Request a partial list of mission items from the system/component.
                http://qgroundcontrol.org/mavlink/waypoint_protocol.
                If start and end index are the same, just send one
                waypoint.

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                start_index               : Start index, 0 by default (int16_t)
                end_index                 : End index, -1 by default (-1: send list to end). Else a valid index of the list (int16_t)

                '''
                return self.send(self.mission_request_partial_list_encode(target_system, target_component, start_index, end_index))

        def mission_write_partial_list_encode(self, target_system, target_component, start_index, end_index):
                '''
                This message is sent to the MAV to write a partial list. If start
                index == end index, only one item will be transmitted
                / updated. If the start index is NOT 0 and above the
                current list size, this request should be REJECTED!

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                start_index               : Start index, 0 by default and smaller / equal to the largest index of the current onboard list. (int16_t)
                end_index                 : End index, equal or greater than start index. (int16_t)

                '''
                return MAVLink_mission_write_partial_list_message(target_system, target_component, start_index, end_index)

        def mission_write_partial_list_send(self, target_system, target_component, start_index, end_index):
                '''
                This message is sent to the MAV to write a partial list. If start
                index == end index, only one item will be transmitted
                / updated. If the start index is NOT 0 and above the
                current list size, this request should be REJECTED!

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                start_index               : Start index, 0 by default and smaller / equal to the largest index of the current onboard list. (int16_t)
                end_index                 : End index, equal or greater than start index. (int16_t)

                '''
                return self.send(self.mission_write_partial_list_encode(target_system, target_component, start_index, end_index))

        def mission_item_encode(self, target_system, target_component, seq, frame, command, current, autocontinue, param1, param2, param3, param4, x, y, z):
                '''
                Message encoding a mission item. This message is emitted to announce
                the presence of a mission item and to set a mission
                item on the system. The mission item can be either in
                x, y, z meters (type: LOCAL) or x:lat, y:lon,
                z:altitude. Local frame is Z-down, right handed (NED),
                global frame is Z-up, right handed (ENU). See also
                http://qgroundcontrol.org/mavlink/waypoint_protocol.

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                seq                       : Sequence (uint16_t)
                frame                     : The coordinate system of the MISSION. see MAV_FRAME in mavlink_types.h (uint8_t)
                command                   : The scheduled action for the MISSION. see MAV_CMD in common.xml MAVLink specs (uint16_t)
                current                   : false:0, true:1 (uint8_t)
                autocontinue              : autocontinue to next wp (uint8_t)
                param1                    : PARAM1, see MAV_CMD enum (float)
                param2                    : PARAM2, see MAV_CMD enum (float)
                param3                    : PARAM3, see MAV_CMD enum (float)
                param4                    : PARAM4, see MAV_CMD enum (float)
                x                         : PARAM5 / local: x position, global: latitude (float)
                y                         : PARAM6 / y position: global: longitude (float)
                z                         : PARAM7 / z position: global: altitude (relative or absolute, depending on frame. (float)

                '''
                return MAVLink_mission_item_message(target_system, target_component, seq, frame, command, current, autocontinue, param1, param2, param3, param4, x, y, z)

        def mission_item_send(self, target_system, target_component, seq, frame, command, current, autocontinue, param1, param2, param3, param4, x, y, z):
                '''
                Message encoding a mission item. This message is emitted to announce
                the presence of a mission item and to set a mission
                item on the system. The mission item can be either in
                x, y, z meters (type: LOCAL) or x:lat, y:lon,
                z:altitude. Local frame is Z-down, right handed (NED),
                global frame is Z-up, right handed (ENU). See also
                http://qgroundcontrol.org/mavlink/waypoint_protocol.

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                seq                       : Sequence (uint16_t)
                frame                     : The coordinate system of the MISSION. see MAV_FRAME in mavlink_types.h (uint8_t)
                command                   : The scheduled action for the MISSION. see MAV_CMD in common.xml MAVLink specs (uint16_t)
                current                   : false:0, true:1 (uint8_t)
                autocontinue              : autocontinue to next wp (uint8_t)
                param1                    : PARAM1, see MAV_CMD enum (float)
                param2                    : PARAM2, see MAV_CMD enum (float)
                param3                    : PARAM3, see MAV_CMD enum (float)
                param4                    : PARAM4, see MAV_CMD enum (float)
                x                         : PARAM5 / local: x position, global: latitude (float)
                y                         : PARAM6 / y position: global: longitude (float)
                z                         : PARAM7 / z position: global: altitude (relative or absolute, depending on frame. (float)

                '''
                return self.send(self.mission_item_encode(target_system, target_component, seq, frame, command, current, autocontinue, param1, param2, param3, param4, x, y, z))

        def mission_request_encode(self, target_system, target_component, seq):
                '''
                Request the information of the mission item with the sequence number
                seq. The response of the system to this message should
                be a MISSION_ITEM message.
                http://qgroundcontrol.org/mavlink/waypoint_protocol

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                seq                       : Sequence (uint16_t)

                '''
                return MAVLink_mission_request_message(target_system, target_component, seq)

        def mission_request_send(self, target_system, target_component, seq):
                '''
                Request the information of the mission item with the sequence number
                seq. The response of the system to this message should
                be a MISSION_ITEM message.
                http://qgroundcontrol.org/mavlink/waypoint_protocol

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                seq                       : Sequence (uint16_t)

                '''
                return self.send(self.mission_request_encode(target_system, target_component, seq))

        def mission_set_current_encode(self, target_system, target_component, seq):
                '''
                Set the mission item with sequence number seq as current item. This
                means that the MAV will continue to this mission item
                on the shortest path (not following the mission items
                in-between).

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                seq                       : Sequence (uint16_t)

                '''
                return MAVLink_mission_set_current_message(target_system, target_component, seq)

        def mission_set_current_send(self, target_system, target_component, seq):
                '''
                Set the mission item with sequence number seq as current item. This
                means that the MAV will continue to this mission item
                on the shortest path (not following the mission items
                in-between).

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                seq                       : Sequence (uint16_t)

                '''
                return self.send(self.mission_set_current_encode(target_system, target_component, seq))

        def mission_current_encode(self, seq):
                '''
                Message that announces the sequence number of the current active
                mission item. The MAV will fly towards this mission
                item.

                seq                       : Sequence (uint16_t)

                '''
                return MAVLink_mission_current_message(seq)

        def mission_current_send(self, seq):
                '''
                Message that announces the sequence number of the current active
                mission item. The MAV will fly towards this mission
                item.

                seq                       : Sequence (uint16_t)

                '''
                return self.send(self.mission_current_encode(seq))

        def mission_request_list_encode(self, target_system, target_component):
                '''
                Request the overall list of mission items from the system/component.

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)

                '''
                return MAVLink_mission_request_list_message(target_system, target_component)

        def mission_request_list_send(self, target_system, target_component):
                '''
                Request the overall list of mission items from the system/component.

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)

                '''
                return self.send(self.mission_request_list_encode(target_system, target_component))

        def mission_count_encode(self, target_system, target_component, count):
                '''
                This message is emitted as response to MISSION_REQUEST_LIST by the MAV
                and to initiate a write transaction. The GCS can then
                request the individual mission item based on the
                knowledge of the total number of MISSIONs.

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                count                     : Number of mission items in the sequence (uint16_t)

                '''
                return MAVLink_mission_count_message(target_system, target_component, count)

        def mission_count_send(self, target_system, target_component, count):
                '''
                This message is emitted as response to MISSION_REQUEST_LIST by the MAV
                and to initiate a write transaction. The GCS can then
                request the individual mission item based on the
                knowledge of the total number of MISSIONs.

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                count                     : Number of mission items in the sequence (uint16_t)

                '''
                return self.send(self.mission_count_encode(target_system, target_component, count))

        def mission_clear_all_encode(self, target_system, target_component):
                '''
                Delete all mission items at once.

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)

                '''
                return MAVLink_mission_clear_all_message(target_system, target_component)

        def mission_clear_all_send(self, target_system, target_component):
                '''
                Delete all mission items at once.

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)

                '''
                return self.send(self.mission_clear_all_encode(target_system, target_component))

        def mission_item_reached_encode(self, seq):
                '''
                A certain mission item has been reached. The system will either hold
                this position (or circle on the orbit) or (if the
                autocontinue on the WP was set) continue to the next
                MISSION.

                seq                       : Sequence (uint16_t)

                '''
                return MAVLink_mission_item_reached_message(seq)

        def mission_item_reached_send(self, seq):
                '''
                A certain mission item has been reached. The system will either hold
                this position (or circle on the orbit) or (if the
                autocontinue on the WP was set) continue to the next
                MISSION.

                seq                       : Sequence (uint16_t)

                '''
                return self.send(self.mission_item_reached_encode(seq))

        def mission_ack_encode(self, target_system, target_component, type):
                '''
                Ack message during MISSION handling. The type field states if this
                message is a positive ack (type=0) or if an error
                happened (type=non-zero).

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                type                      : See MAV_MISSION_RESULT enum (uint8_t)

                '''
                return MAVLink_mission_ack_message(target_system, target_component, type)

        def mission_ack_send(self, target_system, target_component, type):
                '''
                Ack message during MISSION handling. The type field states if this
                message is a positive ack (type=0) or if an error
                happened (type=non-zero).

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                type                      : See MAV_MISSION_RESULT enum (uint8_t)

                '''
                return self.send(self.mission_ack_encode(target_system, target_component, type))

        def set_gps_global_origin_encode(self, target_system, latitude, longitude, altitude):
                '''
                As local waypoints exist, the global MISSION reference allows to
                transform between the local coordinate frame and the
                global (GPS) coordinate frame. This can be necessary
                when e.g. in- and outdoor settings are connected and
                the MAV should move from in- to outdoor.

                target_system             : System ID (uint8_t)
                latitude                  : Latitude (WGS84), in degrees * 1E7 (int32_t)
                longitude                 : Longitude (WGS84, in degrees * 1E7 (int32_t)
                altitude                  : Altitude (AMSL), in meters * 1000 (positive for up) (int32_t)

                '''
                return MAVLink_set_gps_global_origin_message(target_system, latitude, longitude, altitude)

        def set_gps_global_origin_send(self, target_system, latitude, longitude, altitude):
                '''
                As local waypoints exist, the global MISSION reference allows to
                transform between the local coordinate frame and the
                global (GPS) coordinate frame. This can be necessary
                when e.g. in- and outdoor settings are connected and
                the MAV should move from in- to outdoor.

                target_system             : System ID (uint8_t)
                latitude                  : Latitude (WGS84), in degrees * 1E7 (int32_t)
                longitude                 : Longitude (WGS84, in degrees * 1E7 (int32_t)
                altitude                  : Altitude (AMSL), in meters * 1000 (positive for up) (int32_t)

                '''
                return self.send(self.set_gps_global_origin_encode(target_system, latitude, longitude, altitude))

        def gps_global_origin_encode(self, latitude, longitude, altitude):
                '''
                Once the MAV sets a new GPS-Local correspondence, this message
                announces the origin (0,0,0) position

                latitude                  : Latitude (WGS84), in degrees * 1E7 (int32_t)
                longitude                 : Longitude (WGS84), in degrees * 1E7 (int32_t)
                altitude                  : Altitude (AMSL), in meters * 1000 (positive for up) (int32_t)

                '''
                return MAVLink_gps_global_origin_message(latitude, longitude, altitude)

        def gps_global_origin_send(self, latitude, longitude, altitude):
                '''
                Once the MAV sets a new GPS-Local correspondence, this message
                announces the origin (0,0,0) position

                latitude                  : Latitude (WGS84), in degrees * 1E7 (int32_t)
                longitude                 : Longitude (WGS84), in degrees * 1E7 (int32_t)
                altitude                  : Altitude (AMSL), in meters * 1000 (positive for up) (int32_t)

                '''
                return self.send(self.gps_global_origin_encode(latitude, longitude, altitude))

        def param_map_rc_encode(self, target_system, target_component, param_id, param_index, parameter_rc_channel_index, param_value0, scale, param_value_min, param_value_max):
                '''
                Bind a RC channel to a parameter. The parameter should change accoding
                to the RC channel value.

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                param_id                  : Onboard parameter id, terminated by NULL if the length is less than 16 human-readable chars and WITHOUT null termination (NULL) byte if the length is exactly 16 chars - applications have to provide 16+1 bytes storage if the ID is stored as string (char)
                param_index               : Parameter index. Send -1 to use the param ID field as identifier (else the param id will be ignored), send -2 to disable any existing map for this rc_channel_index. (int16_t)
                parameter_rc_channel_index        : Index of parameter RC channel. Not equal to the RC channel id. Typically correpsonds to a potentiometer-knob on the RC. (uint8_t)
                param_value0              : Initial parameter value (float)
                scale                     : Scale, maps the RC range [-1, 1] to a parameter value (float)
                param_value_min           : Minimum param value. The protocol does not define if this overwrites an onboard minimum value. (Depends on implementation) (float)
                param_value_max           : Maximum param value. The protocol does not define if this overwrites an onboard maximum value. (Depends on implementation) (float)

                '''
                return MAVLink_param_map_rc_message(target_system, target_component, param_id, param_index, parameter_rc_channel_index, param_value0, scale, param_value_min, param_value_max)

        def param_map_rc_send(self, target_system, target_component, param_id, param_index, parameter_rc_channel_index, param_value0, scale, param_value_min, param_value_max):
                '''
                Bind a RC channel to a parameter. The parameter should change accoding
                to the RC channel value.

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                param_id                  : Onboard parameter id, terminated by NULL if the length is less than 16 human-readable chars and WITHOUT null termination (NULL) byte if the length is exactly 16 chars - applications have to provide 16+1 bytes storage if the ID is stored as string (char)
                param_index               : Parameter index. Send -1 to use the param ID field as identifier (else the param id will be ignored), send -2 to disable any existing map for this rc_channel_index. (int16_t)
                parameter_rc_channel_index        : Index of parameter RC channel. Not equal to the RC channel id. Typically correpsonds to a potentiometer-knob on the RC. (uint8_t)
                param_value0              : Initial parameter value (float)
                scale                     : Scale, maps the RC range [-1, 1] to a parameter value (float)
                param_value_min           : Minimum param value. The protocol does not define if this overwrites an onboard minimum value. (Depends on implementation) (float)
                param_value_max           : Maximum param value. The protocol does not define if this overwrites an onboard maximum value. (Depends on implementation) (float)

                '''
                return self.send(self.param_map_rc_encode(target_system, target_component, param_id, param_index, parameter_rc_channel_index, param_value0, scale, param_value_min, param_value_max))

        def safety_set_allowed_area_encode(self, target_system, target_component, frame, p1x, p1y, p1z, p2x, p2y, p2z):
                '''
                Set a safety zone (volume), which is defined by two corners of a cube.
                This message can be used to tell the MAV which
                setpoints/MISSIONs to accept and which to reject.
                Safety areas are often enforced by national or
                competition regulations.

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                frame                     : Coordinate frame, as defined by MAV_FRAME enum in mavlink_types.h. Can be either global, GPS, right-handed with Z axis up or local, right handed, Z axis down. (uint8_t)
                p1x                       : x position 1 / Latitude 1 (float)
                p1y                       : y position 1 / Longitude 1 (float)
                p1z                       : z position 1 / Altitude 1 (float)
                p2x                       : x position 2 / Latitude 2 (float)
                p2y                       : y position 2 / Longitude 2 (float)
                p2z                       : z position 2 / Altitude 2 (float)

                '''
                return MAVLink_safety_set_allowed_area_message(target_system, target_component, frame, p1x, p1y, p1z, p2x, p2y, p2z)

        def safety_set_allowed_area_send(self, target_system, target_component, frame, p1x, p1y, p1z, p2x, p2y, p2z):
                '''
                Set a safety zone (volume), which is defined by two corners of a cube.
                This message can be used to tell the MAV which
                setpoints/MISSIONs to accept and which to reject.
                Safety areas are often enforced by national or
                competition regulations.

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                frame                     : Coordinate frame, as defined by MAV_FRAME enum in mavlink_types.h. Can be either global, GPS, right-handed with Z axis up or local, right handed, Z axis down. (uint8_t)
                p1x                       : x position 1 / Latitude 1 (float)
                p1y                       : y position 1 / Longitude 1 (float)
                p1z                       : z position 1 / Altitude 1 (float)
                p2x                       : x position 2 / Latitude 2 (float)
                p2y                       : y position 2 / Longitude 2 (float)
                p2z                       : z position 2 / Altitude 2 (float)

                '''
                return self.send(self.safety_set_allowed_area_encode(target_system, target_component, frame, p1x, p1y, p1z, p2x, p2y, p2z))

        def safety_allowed_area_encode(self, frame, p1x, p1y, p1z, p2x, p2y, p2z):
                '''
                Read out the safety zone the MAV currently assumes.

                frame                     : Coordinate frame, as defined by MAV_FRAME enum in mavlink_types.h. Can be either global, GPS, right-handed with Z axis up or local, right handed, Z axis down. (uint8_t)
                p1x                       : x position 1 / Latitude 1 (float)
                p1y                       : y position 1 / Longitude 1 (float)
                p1z                       : z position 1 / Altitude 1 (float)
                p2x                       : x position 2 / Latitude 2 (float)
                p2y                       : y position 2 / Longitude 2 (float)
                p2z                       : z position 2 / Altitude 2 (float)

                '''
                return MAVLink_safety_allowed_area_message(frame, p1x, p1y, p1z, p2x, p2y, p2z)

        def safety_allowed_area_send(self, frame, p1x, p1y, p1z, p2x, p2y, p2z):
                '''
                Read out the safety zone the MAV currently assumes.

                frame                     : Coordinate frame, as defined by MAV_FRAME enum in mavlink_types.h. Can be either global, GPS, right-handed with Z axis up or local, right handed, Z axis down. (uint8_t)
                p1x                       : x position 1 / Latitude 1 (float)
                p1y                       : y position 1 / Longitude 1 (float)
                p1z                       : z position 1 / Altitude 1 (float)
                p2x                       : x position 2 / Latitude 2 (float)
                p2y                       : y position 2 / Longitude 2 (float)
                p2z                       : z position 2 / Altitude 2 (float)

                '''
                return self.send(self.safety_allowed_area_encode(frame, p1x, p1y, p1z, p2x, p2y, p2z))

        def attitude_quaternion_cov_encode(self, time_boot_ms, q, rollspeed, pitchspeed, yawspeed, covariance):
                '''
                The attitude in the aeronautical frame (right-handed, Z-down, X-front,
                Y-right), expressed as quaternion. Quaternion order is
                w, x, y, z and a zero rotation would be expressed as
                (1 0 0 0).

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                q                         : Quaternion components, w, x, y, z (1 0 0 0 is the null-rotation) (float)
                rollspeed                 : Roll angular speed (rad/s) (float)
                pitchspeed                : Pitch angular speed (rad/s) (float)
                yawspeed                  : Yaw angular speed (rad/s) (float)
                covariance                : Attitude covariance (float)

                '''
                return MAVLink_attitude_quaternion_cov_message(time_boot_ms, q, rollspeed, pitchspeed, yawspeed, covariance)

        def attitude_quaternion_cov_send(self, time_boot_ms, q, rollspeed, pitchspeed, yawspeed, covariance):
                '''
                The attitude in the aeronautical frame (right-handed, Z-down, X-front,
                Y-right), expressed as quaternion. Quaternion order is
                w, x, y, z and a zero rotation would be expressed as
                (1 0 0 0).

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                q                         : Quaternion components, w, x, y, z (1 0 0 0 is the null-rotation) (float)
                rollspeed                 : Roll angular speed (rad/s) (float)
                pitchspeed                : Pitch angular speed (rad/s) (float)
                yawspeed                  : Yaw angular speed (rad/s) (float)
                covariance                : Attitude covariance (float)

                '''
                return self.send(self.attitude_quaternion_cov_encode(time_boot_ms, q, rollspeed, pitchspeed, yawspeed, covariance))

        def nav_controller_output_encode(self, nav_roll, nav_pitch, nav_bearing, target_bearing, wp_dist, alt_error, aspd_error, xtrack_error):
                '''
                Outputs of the APM navigation controller. The primary use of this
                message is to check the response and signs of the
                controller before actual flight and to assist with
                tuning controller parameters.

                nav_roll                  : Current desired roll in degrees (float)
                nav_pitch                 : Current desired pitch in degrees (float)
                nav_bearing               : Current desired heading in degrees (int16_t)
                target_bearing            : Bearing to current MISSION/target in degrees (int16_t)
                wp_dist                   : Distance to active MISSION in meters (uint16_t)
                alt_error                 : Current altitude error in meters (float)
                aspd_error                : Current airspeed error in meters/second (float)
                xtrack_error              : Current crosstrack error on x-y plane in meters (float)

                '''
                return MAVLink_nav_controller_output_message(nav_roll, nav_pitch, nav_bearing, target_bearing, wp_dist, alt_error, aspd_error, xtrack_error)

        def nav_controller_output_send(self, nav_roll, nav_pitch, nav_bearing, target_bearing, wp_dist, alt_error, aspd_error, xtrack_error):
                '''
                Outputs of the APM navigation controller. The primary use of this
                message is to check the response and signs of the
                controller before actual flight and to assist with
                tuning controller parameters.

                nav_roll                  : Current desired roll in degrees (float)
                nav_pitch                 : Current desired pitch in degrees (float)
                nav_bearing               : Current desired heading in degrees (int16_t)
                target_bearing            : Bearing to current MISSION/target in degrees (int16_t)
                wp_dist                   : Distance to active MISSION in meters (uint16_t)
                alt_error                 : Current altitude error in meters (float)
                aspd_error                : Current airspeed error in meters/second (float)
                xtrack_error              : Current crosstrack error on x-y plane in meters (float)

                '''
                return self.send(self.nav_controller_output_encode(nav_roll, nav_pitch, nav_bearing, target_bearing, wp_dist, alt_error, aspd_error, xtrack_error))

        def global_position_int_cov_encode(self, time_boot_ms, time_utc, estimator_type, lat, lon, alt, relative_alt, vx, vy, vz, covariance):
                '''
                The filtered global position (e.g. fused GPS and accelerometers). The
                position is in GPS-frame (right-handed, Z-up). It  is
                designed as scaled integer message since the
                resolution of float is not sufficient. NOTE: This
                message is intended for onboard networks / companion
                computers and higher-bandwidth links and optimized for
                accuracy and completeness. Please use the
                GLOBAL_POSITION_INT message for a minimal subset.

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                time_utc                  : Timestamp (microseconds since UNIX epoch) in UTC. 0 for unknown. Commonly filled by the precision time source of a GPS receiver. (uint64_t)
                estimator_type            : Class id of the estimator this estimate originated from. (uint8_t)
                lat                       : Latitude, expressed as degrees * 1E7 (int32_t)
                lon                       : Longitude, expressed as degrees * 1E7 (int32_t)
                alt                       : Altitude in meters, expressed as * 1000 (millimeters), above MSL (int32_t)
                relative_alt              : Altitude above ground in meters, expressed as * 1000 (millimeters) (int32_t)
                vx                        : Ground X Speed (Latitude), expressed as m/s (float)
                vy                        : Ground Y Speed (Longitude), expressed as m/s (float)
                vz                        : Ground Z Speed (Altitude), expressed as m/s (float)
                covariance                : Covariance matrix (first six entries are the first ROW, next six entries are the second row, etc.) (float)

                '''
                return MAVLink_global_position_int_cov_message(time_boot_ms, time_utc, estimator_type, lat, lon, alt, relative_alt, vx, vy, vz, covariance)

        def global_position_int_cov_send(self, time_boot_ms, time_utc, estimator_type, lat, lon, alt, relative_alt, vx, vy, vz, covariance):
                '''
                The filtered global position (e.g. fused GPS and accelerometers). The
                position is in GPS-frame (right-handed, Z-up). It  is
                designed as scaled integer message since the
                resolution of float is not sufficient. NOTE: This
                message is intended for onboard networks / companion
                computers and higher-bandwidth links and optimized for
                accuracy and completeness. Please use the
                GLOBAL_POSITION_INT message for a minimal subset.

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                time_utc                  : Timestamp (microseconds since UNIX epoch) in UTC. 0 for unknown. Commonly filled by the precision time source of a GPS receiver. (uint64_t)
                estimator_type            : Class id of the estimator this estimate originated from. (uint8_t)
                lat                       : Latitude, expressed as degrees * 1E7 (int32_t)
                lon                       : Longitude, expressed as degrees * 1E7 (int32_t)
                alt                       : Altitude in meters, expressed as * 1000 (millimeters), above MSL (int32_t)
                relative_alt              : Altitude above ground in meters, expressed as * 1000 (millimeters) (int32_t)
                vx                        : Ground X Speed (Latitude), expressed as m/s (float)
                vy                        : Ground Y Speed (Longitude), expressed as m/s (float)
                vz                        : Ground Z Speed (Altitude), expressed as m/s (float)
                covariance                : Covariance matrix (first six entries are the first ROW, next six entries are the second row, etc.) (float)

                '''
                return self.send(self.global_position_int_cov_encode(time_boot_ms, time_utc, estimator_type, lat, lon, alt, relative_alt, vx, vy, vz, covariance))

        def local_position_ned_cov_encode(self, time_boot_ms, time_utc, estimator_type, x, y, z, vx, vy, vz, ax, ay, az, covariance):
                '''
                The filtered local position (e.g. fused computer vision and
                accelerometers). Coordinate frame is right-handed,
                Z-axis down (aeronautical frame, NED / north-east-down
                convention)

                time_boot_ms              : Timestamp (milliseconds since system boot). 0 for system without monotonic timestamp (uint32_t)
                time_utc                  : Timestamp (microseconds since UNIX epoch) in UTC. 0 for unknown. Commonly filled by the precision time source of a GPS receiver. (uint64_t)
                estimator_type            : Class id of the estimator this estimate originated from. (uint8_t)
                x                         : X Position (float)
                y                         : Y Position (float)
                z                         : Z Position (float)
                vx                        : X Speed (m/s) (float)
                vy                        : Y Speed (m/s) (float)
                vz                        : Z Speed (m/s) (float)
                ax                        : X Acceleration (m/s^2) (float)
                ay                        : Y Acceleration (m/s^2) (float)
                az                        : Z Acceleration (m/s^2) (float)
                covariance                : Covariance matrix upper right triangular (first nine entries are the first ROW, next eight entries are the second row, etc.) (float)

                '''
                return MAVLink_local_position_ned_cov_message(time_boot_ms, time_utc, estimator_type, x, y, z, vx, vy, vz, ax, ay, az, covariance)

        def local_position_ned_cov_send(self, time_boot_ms, time_utc, estimator_type, x, y, z, vx, vy, vz, ax, ay, az, covariance):
                '''
                The filtered local position (e.g. fused computer vision and
                accelerometers). Coordinate frame is right-handed,
                Z-axis down (aeronautical frame, NED / north-east-down
                convention)

                time_boot_ms              : Timestamp (milliseconds since system boot). 0 for system without monotonic timestamp (uint32_t)
                time_utc                  : Timestamp (microseconds since UNIX epoch) in UTC. 0 for unknown. Commonly filled by the precision time source of a GPS receiver. (uint64_t)
                estimator_type            : Class id of the estimator this estimate originated from. (uint8_t)
                x                         : X Position (float)
                y                         : Y Position (float)
                z                         : Z Position (float)
                vx                        : X Speed (m/s) (float)
                vy                        : Y Speed (m/s) (float)
                vz                        : Z Speed (m/s) (float)
                ax                        : X Acceleration (m/s^2) (float)
                ay                        : Y Acceleration (m/s^2) (float)
                az                        : Z Acceleration (m/s^2) (float)
                covariance                : Covariance matrix upper right triangular (first nine entries are the first ROW, next eight entries are the second row, etc.) (float)

                '''
                return self.send(self.local_position_ned_cov_encode(time_boot_ms, time_utc, estimator_type, x, y, z, vx, vy, vz, ax, ay, az, covariance))

        def rc_channels_encode(self, time_boot_ms, chancount, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw, chan9_raw, chan10_raw, chan11_raw, chan12_raw, chan13_raw, chan14_raw, chan15_raw, chan16_raw, chan17_raw, chan18_raw, rssi):
                '''
                The PPM values of the RC channels received. The standard PPM
                modulation is as follows: 1000 microseconds: 0%, 2000
                microseconds: 100%. Individual receivers/transmitters
                might violate this specification.

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                chancount                 : Total number of RC channels being received. This can be larger than 18, indicating that more channels are available but not given in this message. This value should be 0 when no RC channels are available. (uint8_t)
                chan1_raw                 : RC channel 1 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan2_raw                 : RC channel 2 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan3_raw                 : RC channel 3 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan4_raw                 : RC channel 4 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan5_raw                 : RC channel 5 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan6_raw                 : RC channel 6 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan7_raw                 : RC channel 7 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan8_raw                 : RC channel 8 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan9_raw                 : RC channel 9 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan10_raw                : RC channel 10 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan11_raw                : RC channel 11 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan12_raw                : RC channel 12 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan13_raw                : RC channel 13 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan14_raw                : RC channel 14 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan15_raw                : RC channel 15 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan16_raw                : RC channel 16 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan17_raw                : RC channel 17 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan18_raw                : RC channel 18 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                rssi                      : Receive signal strength indicator, 0: 0%, 100: 100%, 255: invalid/unknown. (uint8_t)

                '''
                return MAVLink_rc_channels_message(time_boot_ms, chancount, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw, chan9_raw, chan10_raw, chan11_raw, chan12_raw, chan13_raw, chan14_raw, chan15_raw, chan16_raw, chan17_raw, chan18_raw, rssi)

        def rc_channels_send(self, time_boot_ms, chancount, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw, chan9_raw, chan10_raw, chan11_raw, chan12_raw, chan13_raw, chan14_raw, chan15_raw, chan16_raw, chan17_raw, chan18_raw, rssi):
                '''
                The PPM values of the RC channels received. The standard PPM
                modulation is as follows: 1000 microseconds: 0%, 2000
                microseconds: 100%. Individual receivers/transmitters
                might violate this specification.

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                chancount                 : Total number of RC channels being received. This can be larger than 18, indicating that more channels are available but not given in this message. This value should be 0 when no RC channels are available. (uint8_t)
                chan1_raw                 : RC channel 1 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan2_raw                 : RC channel 2 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan3_raw                 : RC channel 3 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan4_raw                 : RC channel 4 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan5_raw                 : RC channel 5 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan6_raw                 : RC channel 6 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan7_raw                 : RC channel 7 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan8_raw                 : RC channel 8 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan9_raw                 : RC channel 9 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan10_raw                : RC channel 10 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan11_raw                : RC channel 11 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan12_raw                : RC channel 12 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan13_raw                : RC channel 13 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan14_raw                : RC channel 14 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan15_raw                : RC channel 15 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan16_raw                : RC channel 16 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan17_raw                : RC channel 17 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                chan18_raw                : RC channel 18 value, in microseconds. A value of UINT16_MAX implies the channel is unused. (uint16_t)
                rssi                      : Receive signal strength indicator, 0: 0%, 100: 100%, 255: invalid/unknown. (uint8_t)

                '''
                return self.send(self.rc_channels_encode(time_boot_ms, chancount, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw, chan9_raw, chan10_raw, chan11_raw, chan12_raw, chan13_raw, chan14_raw, chan15_raw, chan16_raw, chan17_raw, chan18_raw, rssi))

        def request_data_stream_encode(self, target_system, target_component, req_stream_id, req_message_rate, start_stop):
                '''
                

                target_system             : The target requested to send the message stream. (uint8_t)
                target_component          : The target requested to send the message stream. (uint8_t)
                req_stream_id             : The ID of the requested data stream (uint8_t)
                req_message_rate          : The requested interval between two messages of this type (uint16_t)
                start_stop                : 1 to start sending, 0 to stop sending. (uint8_t)

                '''
                return MAVLink_request_data_stream_message(target_system, target_component, req_stream_id, req_message_rate, start_stop)

        def request_data_stream_send(self, target_system, target_component, req_stream_id, req_message_rate, start_stop):
                '''
                

                target_system             : The target requested to send the message stream. (uint8_t)
                target_component          : The target requested to send the message stream. (uint8_t)
                req_stream_id             : The ID of the requested data stream (uint8_t)
                req_message_rate          : The requested interval between two messages of this type (uint16_t)
                start_stop                : 1 to start sending, 0 to stop sending. (uint8_t)

                '''
                return self.send(self.request_data_stream_encode(target_system, target_component, req_stream_id, req_message_rate, start_stop))

        def data_stream_encode(self, stream_id, message_rate, on_off):
                '''
                

                stream_id                 : The ID of the requested data stream (uint8_t)
                message_rate              : The requested interval between two messages of this type (uint16_t)
                on_off                    : 1 stream is enabled, 0 stream is stopped. (uint8_t)

                '''
                return MAVLink_data_stream_message(stream_id, message_rate, on_off)

        def data_stream_send(self, stream_id, message_rate, on_off):
                '''
                

                stream_id                 : The ID of the requested data stream (uint8_t)
                message_rate              : The requested interval between two messages of this type (uint16_t)
                on_off                    : 1 stream is enabled, 0 stream is stopped. (uint8_t)

                '''
                return self.send(self.data_stream_encode(stream_id, message_rate, on_off))

        def manual_control_encode(self, target, x, y, z, r, buttons):
                '''
                This message provides an API for manually controlling the vehicle
                using standard joystick axes nomenclature, along with
                a joystick-like input device. Unused axes can be
                disabled an buttons are also transmit as boolean
                values of their

                target                    : The system to be controlled. (uint8_t)
                x                         : X-axis, normalized to the range [-1000,1000]. A value of INT16_MAX indicates that this axis is invalid. Generally corresponds to forward(1000)-backward(-1000) movement on a joystick and the pitch of a vehicle. (int16_t)
                y                         : Y-axis, normalized to the range [-1000,1000]. A value of INT16_MAX indicates that this axis is invalid. Generally corresponds to left(-1000)-right(1000) movement on a joystick and the roll of a vehicle. (int16_t)
                z                         : Z-axis, normalized to the range [-1000,1000]. A value of INT16_MAX indicates that this axis is invalid. Generally corresponds to a separate slider movement with maximum being 1000 and minimum being -1000 on a joystick and the thrust of a vehicle. (int16_t)
                r                         : R-axis, normalized to the range [-1000,1000]. A value of INT16_MAX indicates that this axis is invalid. Generally corresponds to a twisting of the joystick, with counter-clockwise being 1000 and clockwise being -1000, and the yaw of a vehicle. (int16_t)
                buttons                   : A bitfield corresponding to the joystick buttons' current state, 1 for pressed, 0 for released. The lowest bit corresponds to Button 1. (uint16_t)

                '''
                return MAVLink_manual_control_message(target, x, y, z, r, buttons)

        def manual_control_send(self, target, x, y, z, r, buttons):
                '''
                This message provides an API for manually controlling the vehicle
                using standard joystick axes nomenclature, along with
                a joystick-like input device. Unused axes can be
                disabled an buttons are also transmit as boolean
                values of their

                target                    : The system to be controlled. (uint8_t)
                x                         : X-axis, normalized to the range [-1000,1000]. A value of INT16_MAX indicates that this axis is invalid. Generally corresponds to forward(1000)-backward(-1000) movement on a joystick and the pitch of a vehicle. (int16_t)
                y                         : Y-axis, normalized to the range [-1000,1000]. A value of INT16_MAX indicates that this axis is invalid. Generally corresponds to left(-1000)-right(1000) movement on a joystick and the roll of a vehicle. (int16_t)
                z                         : Z-axis, normalized to the range [-1000,1000]. A value of INT16_MAX indicates that this axis is invalid. Generally corresponds to a separate slider movement with maximum being 1000 and minimum being -1000 on a joystick and the thrust of a vehicle. (int16_t)
                r                         : R-axis, normalized to the range [-1000,1000]. A value of INT16_MAX indicates that this axis is invalid. Generally corresponds to a twisting of the joystick, with counter-clockwise being 1000 and clockwise being -1000, and the yaw of a vehicle. (int16_t)
                buttons                   : A bitfield corresponding to the joystick buttons' current state, 1 for pressed, 0 for released. The lowest bit corresponds to Button 1. (uint16_t)

                '''
                return self.send(self.manual_control_encode(target, x, y, z, r, buttons))

        def rc_channels_override_encode(self, target_system, target_component, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw):
                '''
                The RAW values of the RC channels sent to the MAV to override info
                received from the RC radio. A value of UINT16_MAX
                means no change to that channel. A value of 0 means
                control of that channel should be released back to the
                RC radio. The standard PPM modulation is as follows:
                1000 microseconds: 0%, 2000 microseconds: 100%.
                Individual receivers/transmitters might violate this
                specification.

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                chan1_raw                 : RC channel 1 value, in microseconds. A value of UINT16_MAX means to ignore this field. (uint16_t)
                chan2_raw                 : RC channel 2 value, in microseconds. A value of UINT16_MAX means to ignore this field. (uint16_t)
                chan3_raw                 : RC channel 3 value, in microseconds. A value of UINT16_MAX means to ignore this field. (uint16_t)
                chan4_raw                 : RC channel 4 value, in microseconds. A value of UINT16_MAX means to ignore this field. (uint16_t)
                chan5_raw                 : RC channel 5 value, in microseconds. A value of UINT16_MAX means to ignore this field. (uint16_t)
                chan6_raw                 : RC channel 6 value, in microseconds. A value of UINT16_MAX means to ignore this field. (uint16_t)
                chan7_raw                 : RC channel 7 value, in microseconds. A value of UINT16_MAX means to ignore this field. (uint16_t)
                chan8_raw                 : RC channel 8 value, in microseconds. A value of UINT16_MAX means to ignore this field. (uint16_t)

                '''
                return MAVLink_rc_channels_override_message(target_system, target_component, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw)

        def rc_channels_override_send(self, target_system, target_component, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw):
                '''
                The RAW values of the RC channels sent to the MAV to override info
                received from the RC radio. A value of UINT16_MAX
                means no change to that channel. A value of 0 means
                control of that channel should be released back to the
                RC radio. The standard PPM modulation is as follows:
                1000 microseconds: 0%, 2000 microseconds: 100%.
                Individual receivers/transmitters might violate this
                specification.

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                chan1_raw                 : RC channel 1 value, in microseconds. A value of UINT16_MAX means to ignore this field. (uint16_t)
                chan2_raw                 : RC channel 2 value, in microseconds. A value of UINT16_MAX means to ignore this field. (uint16_t)
                chan3_raw                 : RC channel 3 value, in microseconds. A value of UINT16_MAX means to ignore this field. (uint16_t)
                chan4_raw                 : RC channel 4 value, in microseconds. A value of UINT16_MAX means to ignore this field. (uint16_t)
                chan5_raw                 : RC channel 5 value, in microseconds. A value of UINT16_MAX means to ignore this field. (uint16_t)
                chan6_raw                 : RC channel 6 value, in microseconds. A value of UINT16_MAX means to ignore this field. (uint16_t)
                chan7_raw                 : RC channel 7 value, in microseconds. A value of UINT16_MAX means to ignore this field. (uint16_t)
                chan8_raw                 : RC channel 8 value, in microseconds. A value of UINT16_MAX means to ignore this field. (uint16_t)

                '''
                return self.send(self.rc_channels_override_encode(target_system, target_component, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw))

        def mission_item_int_encode(self, target_system, target_component, seq, frame, command, current, autocontinue, param1, param2, param3, param4, x, y, z):
                '''
                Message encoding a mission item. This message is emitted to announce
                the presence of a mission item and to set a mission
                item on the system. The mission item can be either in
                x, y, z meters (type: LOCAL) or x:lat, y:lon,
                z:altitude. Local frame is Z-down, right handed (NED),
                global frame is Z-up, right handed (ENU). See alsohttp
                ://qgroundcontrol.org/mavlink/waypoint_protocol.

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                seq                       : Waypoint ID (sequence number). Starts at zero. Increases monotonically for each waypoint, no gaps in the sequence (0,1,2,3,4). (uint16_t)
                frame                     : The coordinate system of the MISSION. see MAV_FRAME in mavlink_types.h (uint8_t)
                command                   : The scheduled action for the MISSION. see MAV_CMD in common.xml MAVLink specs (uint16_t)
                current                   : false:0, true:1 (uint8_t)
                autocontinue              : autocontinue to next wp (uint8_t)
                param1                    : PARAM1, see MAV_CMD enum (float)
                param2                    : PARAM2, see MAV_CMD enum (float)
                param3                    : PARAM3, see MAV_CMD enum (float)
                param4                    : PARAM4, see MAV_CMD enum (float)
                x                         : PARAM5 / local: x position in meters * 1e4, global: latitude in degrees * 10^7 (int32_t)
                y                         : PARAM6 / y position: local: x position in meters * 1e4, global: longitude in degrees *10^7 (int32_t)
                z                         : PARAM7 / z position: global: altitude in meters (relative or absolute, depending on frame. (float)

                '''
                return MAVLink_mission_item_int_message(target_system, target_component, seq, frame, command, current, autocontinue, param1, param2, param3, param4, x, y, z)

        def mission_item_int_send(self, target_system, target_component, seq, frame, command, current, autocontinue, param1, param2, param3, param4, x, y, z):
                '''
                Message encoding a mission item. This message is emitted to announce
                the presence of a mission item and to set a mission
                item on the system. The mission item can be either in
                x, y, z meters (type: LOCAL) or x:lat, y:lon,
                z:altitude. Local frame is Z-down, right handed (NED),
                global frame is Z-up, right handed (ENU). See alsohttp
                ://qgroundcontrol.org/mavlink/waypoint_protocol.

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                seq                       : Waypoint ID (sequence number). Starts at zero. Increases monotonically for each waypoint, no gaps in the sequence (0,1,2,3,4). (uint16_t)
                frame                     : The coordinate system of the MISSION. see MAV_FRAME in mavlink_types.h (uint8_t)
                command                   : The scheduled action for the MISSION. see MAV_CMD in common.xml MAVLink specs (uint16_t)
                current                   : false:0, true:1 (uint8_t)
                autocontinue              : autocontinue to next wp (uint8_t)
                param1                    : PARAM1, see MAV_CMD enum (float)
                param2                    : PARAM2, see MAV_CMD enum (float)
                param3                    : PARAM3, see MAV_CMD enum (float)
                param4                    : PARAM4, see MAV_CMD enum (float)
                x                         : PARAM5 / local: x position in meters * 1e4, global: latitude in degrees * 10^7 (int32_t)
                y                         : PARAM6 / y position: local: x position in meters * 1e4, global: longitude in degrees *10^7 (int32_t)
                z                         : PARAM7 / z position: global: altitude in meters (relative or absolute, depending on frame. (float)

                '''
                return self.send(self.mission_item_int_encode(target_system, target_component, seq, frame, command, current, autocontinue, param1, param2, param3, param4, x, y, z))

        def vfr_hud_encode(self, airspeed, groundspeed, heading, throttle, alt, climb):
                '''
                Metrics typically displayed on a HUD for fixed wing aircraft

                airspeed                  : Current airspeed in m/s (float)
                groundspeed               : Current ground speed in m/s (float)
                heading                   : Current heading in degrees, in compass units (0..360, 0=north) (int16_t)
                throttle                  : Current throttle setting in integer percent, 0 to 100 (uint16_t)
                alt                       : Current altitude (MSL), in meters (float)
                climb                     : Current climb rate in meters/second (float)

                '''
                return MAVLink_vfr_hud_message(airspeed, groundspeed, heading, throttle, alt, climb)

        def vfr_hud_send(self, airspeed, groundspeed, heading, throttle, alt, climb):
                '''
                Metrics typically displayed on a HUD for fixed wing aircraft

                airspeed                  : Current airspeed in m/s (float)
                groundspeed               : Current ground speed in m/s (float)
                heading                   : Current heading in degrees, in compass units (0..360, 0=north) (int16_t)
                throttle                  : Current throttle setting in integer percent, 0 to 100 (uint16_t)
                alt                       : Current altitude (MSL), in meters (float)
                climb                     : Current climb rate in meters/second (float)

                '''
                return self.send(self.vfr_hud_encode(airspeed, groundspeed, heading, throttle, alt, climb))

        def command_int_encode(self, target_system, target_component, frame, command, current, autocontinue, param1, param2, param3, param4, x, y, z):
                '''
                Message encoding a command with parameters as scaled integers. Scaling
                depends on the actual command value.

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                frame                     : The coordinate system of the COMMAND. see MAV_FRAME in mavlink_types.h (uint8_t)
                command                   : The scheduled action for the mission item. see MAV_CMD in common.xml MAVLink specs (uint16_t)
                current                   : false:0, true:1 (uint8_t)
                autocontinue              : autocontinue to next wp (uint8_t)
                param1                    : PARAM1, see MAV_CMD enum (float)
                param2                    : PARAM2, see MAV_CMD enum (float)
                param3                    : PARAM3, see MAV_CMD enum (float)
                param4                    : PARAM4, see MAV_CMD enum (float)
                x                         : PARAM5 / local: x position in meters * 1e4, global: latitude in degrees * 10^7 (int32_t)
                y                         : PARAM6 / local: y position in meters * 1e4, global: longitude in degrees * 10^7 (int32_t)
                z                         : PARAM7 / z position: global: altitude in meters (relative or absolute, depending on frame. (float)

                '''
                return MAVLink_command_int_message(target_system, target_component, frame, command, current, autocontinue, param1, param2, param3, param4, x, y, z)

        def command_int_send(self, target_system, target_component, frame, command, current, autocontinue, param1, param2, param3, param4, x, y, z):
                '''
                Message encoding a command with parameters as scaled integers. Scaling
                depends on the actual command value.

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                frame                     : The coordinate system of the COMMAND. see MAV_FRAME in mavlink_types.h (uint8_t)
                command                   : The scheduled action for the mission item. see MAV_CMD in common.xml MAVLink specs (uint16_t)
                current                   : false:0, true:1 (uint8_t)
                autocontinue              : autocontinue to next wp (uint8_t)
                param1                    : PARAM1, see MAV_CMD enum (float)
                param2                    : PARAM2, see MAV_CMD enum (float)
                param3                    : PARAM3, see MAV_CMD enum (float)
                param4                    : PARAM4, see MAV_CMD enum (float)
                x                         : PARAM5 / local: x position in meters * 1e4, global: latitude in degrees * 10^7 (int32_t)
                y                         : PARAM6 / local: y position in meters * 1e4, global: longitude in degrees * 10^7 (int32_t)
                z                         : PARAM7 / z position: global: altitude in meters (relative or absolute, depending on frame. (float)

                '''
                return self.send(self.command_int_encode(target_system, target_component, frame, command, current, autocontinue, param1, param2, param3, param4, x, y, z))

        def command_long_encode(self, target_system, target_component, command, confirmation, param1, param2, param3, param4, param5, param6, param7):
                '''
                Send a command with up to seven parameters to the MAV

                target_system             : System which should execute the command (uint8_t)
                target_component          : Component which should execute the command, 0 for all components (uint8_t)
                command                   : Command ID, as defined by MAV_CMD enum. (uint16_t)
                confirmation              : 0: First transmission of this command. 1-255: Confirmation transmissions (e.g. for kill command) (uint8_t)
                param1                    : Parameter 1, as defined by MAV_CMD enum. (float)
                param2                    : Parameter 2, as defined by MAV_CMD enum. (float)
                param3                    : Parameter 3, as defined by MAV_CMD enum. (float)
                param4                    : Parameter 4, as defined by MAV_CMD enum. (float)
                param5                    : Parameter 5, as defined by MAV_CMD enum. (float)
                param6                    : Parameter 6, as defined by MAV_CMD enum. (float)
                param7                    : Parameter 7, as defined by MAV_CMD enum. (float)

                '''
                return MAVLink_command_long_message(target_system, target_component, command, confirmation, param1, param2, param3, param4, param5, param6, param7)

        def command_long_send(self, target_system, target_component, command, confirmation, param1, param2, param3, param4, param5, param6, param7):
                '''
                Send a command with up to seven parameters to the MAV

                target_system             : System which should execute the command (uint8_t)
                target_component          : Component which should execute the command, 0 for all components (uint8_t)
                command                   : Command ID, as defined by MAV_CMD enum. (uint16_t)
                confirmation              : 0: First transmission of this command. 1-255: Confirmation transmissions (e.g. for kill command) (uint8_t)
                param1                    : Parameter 1, as defined by MAV_CMD enum. (float)
                param2                    : Parameter 2, as defined by MAV_CMD enum. (float)
                param3                    : Parameter 3, as defined by MAV_CMD enum. (float)
                param4                    : Parameter 4, as defined by MAV_CMD enum. (float)
                param5                    : Parameter 5, as defined by MAV_CMD enum. (float)
                param6                    : Parameter 6, as defined by MAV_CMD enum. (float)
                param7                    : Parameter 7, as defined by MAV_CMD enum. (float)

                '''
                return self.send(self.command_long_encode(target_system, target_component, command, confirmation, param1, param2, param3, param4, param5, param6, param7))

        def command_ack_encode(self, command, result):
                '''
                Report status of a command. Includes feedback wether the command was
                executed.

                command                   : Command ID, as defined by MAV_CMD enum. (uint16_t)
                result                    : See MAV_RESULT enum (uint8_t)

                '''
                return MAVLink_command_ack_message(command, result)

        def command_ack_send(self, command, result):
                '''
                Report status of a command. Includes feedback wether the command was
                executed.

                command                   : Command ID, as defined by MAV_CMD enum. (uint16_t)
                result                    : See MAV_RESULT enum (uint8_t)

                '''
                return self.send(self.command_ack_encode(command, result))

        def manual_setpoint_encode(self, time_boot_ms, roll, pitch, yaw, thrust, mode_switch, manual_override_switch):
                '''
                Setpoint in roll, pitch, yaw and thrust from the operator

                time_boot_ms              : Timestamp in milliseconds since system boot (uint32_t)
                roll                      : Desired roll rate in radians per second (float)
                pitch                     : Desired pitch rate in radians per second (float)
                yaw                       : Desired yaw rate in radians per second (float)
                thrust                    : Collective thrust, normalized to 0 .. 1 (float)
                mode_switch               : Flight mode switch position, 0.. 255 (uint8_t)
                manual_override_switch        : Override mode switch position, 0.. 255 (uint8_t)

                '''
                return MAVLink_manual_setpoint_message(time_boot_ms, roll, pitch, yaw, thrust, mode_switch, manual_override_switch)

        def manual_setpoint_send(self, time_boot_ms, roll, pitch, yaw, thrust, mode_switch, manual_override_switch):
                '''
                Setpoint in roll, pitch, yaw and thrust from the operator

                time_boot_ms              : Timestamp in milliseconds since system boot (uint32_t)
                roll                      : Desired roll rate in radians per second (float)
                pitch                     : Desired pitch rate in radians per second (float)
                yaw                       : Desired yaw rate in radians per second (float)
                thrust                    : Collective thrust, normalized to 0 .. 1 (float)
                mode_switch               : Flight mode switch position, 0.. 255 (uint8_t)
                manual_override_switch        : Override mode switch position, 0.. 255 (uint8_t)

                '''
                return self.send(self.manual_setpoint_encode(time_boot_ms, roll, pitch, yaw, thrust, mode_switch, manual_override_switch))

        def set_attitude_target_encode(self, time_boot_ms, target_system, target_component, type_mask, q, body_roll_rate, body_pitch_rate, body_yaw_rate, thrust):
                '''
                Set the vehicle attitude and body angular rates.

                time_boot_ms              : Timestamp in milliseconds since system boot (uint32_t)
                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                type_mask                 : Mappings: If any of these bits are set, the corresponding input should be ignored: bit 1: body roll rate, bit 2: body pitch rate, bit 3: body yaw rate. bit 4-bit 6: reserved, bit 7: throttle, bit 8: attitude (uint8_t)
                q                         : Attitude quaternion (w, x, y, z order, zero-rotation is 1, 0, 0, 0) (float)
                body_roll_rate            : Body roll rate in radians per second (float)
                body_pitch_rate           : Body roll rate in radians per second (float)
                body_yaw_rate             : Body roll rate in radians per second (float)
                thrust                    : Collective thrust, normalized to 0 .. 1 (-1 .. 1 for vehicles capable of reverse trust) (float)

                '''
                return MAVLink_set_attitude_target_message(time_boot_ms, target_system, target_component, type_mask, q, body_roll_rate, body_pitch_rate, body_yaw_rate, thrust)

        def set_attitude_target_send(self, time_boot_ms, target_system, target_component, type_mask, q, body_roll_rate, body_pitch_rate, body_yaw_rate, thrust):
                '''
                Set the vehicle attitude and body angular rates.

                time_boot_ms              : Timestamp in milliseconds since system boot (uint32_t)
                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                type_mask                 : Mappings: If any of these bits are set, the corresponding input should be ignored: bit 1: body roll rate, bit 2: body pitch rate, bit 3: body yaw rate. bit 4-bit 6: reserved, bit 7: throttle, bit 8: attitude (uint8_t)
                q                         : Attitude quaternion (w, x, y, z order, zero-rotation is 1, 0, 0, 0) (float)
                body_roll_rate            : Body roll rate in radians per second (float)
                body_pitch_rate           : Body roll rate in radians per second (float)
                body_yaw_rate             : Body roll rate in radians per second (float)
                thrust                    : Collective thrust, normalized to 0 .. 1 (-1 .. 1 for vehicles capable of reverse trust) (float)

                '''
                return self.send(self.set_attitude_target_encode(time_boot_ms, target_system, target_component, type_mask, q, body_roll_rate, body_pitch_rate, body_yaw_rate, thrust))

        def attitude_target_encode(self, time_boot_ms, type_mask, q, body_roll_rate, body_pitch_rate, body_yaw_rate, thrust):
                '''
                Set the vehicle attitude and body angular rates.

                time_boot_ms              : Timestamp in milliseconds since system boot (uint32_t)
                type_mask                 : Mappings: If any of these bits are set, the corresponding input should be ignored: bit 1: body roll rate, bit 2: body pitch rate, bit 3: body yaw rate. bit 4-bit 7: reserved, bit 8: attitude (uint8_t)
                q                         : Attitude quaternion (w, x, y, z order, zero-rotation is 1, 0, 0, 0) (float)
                body_roll_rate            : Body roll rate in radians per second (float)
                body_pitch_rate           : Body roll rate in radians per second (float)
                body_yaw_rate             : Body roll rate in radians per second (float)
                thrust                    : Collective thrust, normalized to 0 .. 1 (-1 .. 1 for vehicles capable of reverse trust) (float)

                '''
                return MAVLink_attitude_target_message(time_boot_ms, type_mask, q, body_roll_rate, body_pitch_rate, body_yaw_rate, thrust)

        def attitude_target_send(self, time_boot_ms, type_mask, q, body_roll_rate, body_pitch_rate, body_yaw_rate, thrust):
                '''
                Set the vehicle attitude and body angular rates.

                time_boot_ms              : Timestamp in milliseconds since system boot (uint32_t)
                type_mask                 : Mappings: If any of these bits are set, the corresponding input should be ignored: bit 1: body roll rate, bit 2: body pitch rate, bit 3: body yaw rate. bit 4-bit 7: reserved, bit 8: attitude (uint8_t)
                q                         : Attitude quaternion (w, x, y, z order, zero-rotation is 1, 0, 0, 0) (float)
                body_roll_rate            : Body roll rate in radians per second (float)
                body_pitch_rate           : Body roll rate in radians per second (float)
                body_yaw_rate             : Body roll rate in radians per second (float)
                thrust                    : Collective thrust, normalized to 0 .. 1 (-1 .. 1 for vehicles capable of reverse trust) (float)

                '''
                return self.send(self.attitude_target_encode(time_boot_ms, type_mask, q, body_roll_rate, body_pitch_rate, body_yaw_rate, thrust))

        def set_position_target_local_ned_encode(self, time_boot_ms, target_system, target_component, coordinate_frame, type_mask, x, y, z, vx, vy, vz, afx, afy, afz, yaw, yaw_rate):
                '''
                Set vehicle position, velocity and acceleration setpoint in local
                frame.

                time_boot_ms              : Timestamp in milliseconds since system boot (uint32_t)
                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                coordinate_frame          : Valid options are: MAV_FRAME_LOCAL_NED = 1, MAV_FRAME_LOCAL_OFFSET_NED = 7, MAV_FRAME_BODY_NED = 8, MAV_FRAME_BODY_OFFSET_NED = 9 (uint8_t)
                type_mask                 : Bitmask to indicate which dimensions should be ignored by the vehicle: a value of 0b0000000000000000 or 0b0000001000000000 indicates that none of the setpoint dimensions should be ignored. If bit 10 is set the floats afx afy afz should be interpreted as force instead of acceleration. Mapping: bit 1: x, bit 2: y, bit 3: z, bit 4: vx, bit 5: vy, bit 6: vz, bit 7: ax, bit 8: ay, bit 9: az, bit 10: is force setpoint, bit 11: yaw, bit 12: yaw rate (uint16_t)
                x                         : X Position in NED frame in meters (float)
                y                         : Y Position in NED frame in meters (float)
                z                         : Z Position in NED frame in meters (note, altitude is negative in NED) (float)
                vx                        : X velocity in NED frame in meter / s (float)
                vy                        : Y velocity in NED frame in meter / s (float)
                vz                        : Z velocity in NED frame in meter / s (float)
                afx                       : X acceleration or force (if bit 10 of type_mask is set) in NED frame in meter / s^2 or N (float)
                afy                       : Y acceleration or force (if bit 10 of type_mask is set) in NED frame in meter / s^2 or N (float)
                afz                       : Z acceleration or force (if bit 10 of type_mask is set) in NED frame in meter / s^2 or N (float)
                yaw                       : yaw setpoint in rad (float)
                yaw_rate                  : yaw rate setpoint in rad/s (float)

                '''
                return MAVLink_set_position_target_local_ned_message(time_boot_ms, target_system, target_component, coordinate_frame, type_mask, x, y, z, vx, vy, vz, afx, afy, afz, yaw, yaw_rate)

        def set_position_target_local_ned_send(self, time_boot_ms, target_system, target_component, coordinate_frame, type_mask, x, y, z, vx, vy, vz, afx, afy, afz, yaw, yaw_rate):
                '''
                Set vehicle position, velocity and acceleration setpoint in local
                frame.

                time_boot_ms              : Timestamp in milliseconds since system boot (uint32_t)
                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                coordinate_frame          : Valid options are: MAV_FRAME_LOCAL_NED = 1, MAV_FRAME_LOCAL_OFFSET_NED = 7, MAV_FRAME_BODY_NED = 8, MAV_FRAME_BODY_OFFSET_NED = 9 (uint8_t)
                type_mask                 : Bitmask to indicate which dimensions should be ignored by the vehicle: a value of 0b0000000000000000 or 0b0000001000000000 indicates that none of the setpoint dimensions should be ignored. If bit 10 is set the floats afx afy afz should be interpreted as force instead of acceleration. Mapping: bit 1: x, bit 2: y, bit 3: z, bit 4: vx, bit 5: vy, bit 6: vz, bit 7: ax, bit 8: ay, bit 9: az, bit 10: is force setpoint, bit 11: yaw, bit 12: yaw rate (uint16_t)
                x                         : X Position in NED frame in meters (float)
                y                         : Y Position in NED frame in meters (float)
                z                         : Z Position in NED frame in meters (note, altitude is negative in NED) (float)
                vx                        : X velocity in NED frame in meter / s (float)
                vy                        : Y velocity in NED frame in meter / s (float)
                vz                        : Z velocity in NED frame in meter / s (float)
                afx                       : X acceleration or force (if bit 10 of type_mask is set) in NED frame in meter / s^2 or N (float)
                afy                       : Y acceleration or force (if bit 10 of type_mask is set) in NED frame in meter / s^2 or N (float)
                afz                       : Z acceleration or force (if bit 10 of type_mask is set) in NED frame in meter / s^2 or N (float)
                yaw                       : yaw setpoint in rad (float)
                yaw_rate                  : yaw rate setpoint in rad/s (float)

                '''
                return self.send(self.set_position_target_local_ned_encode(time_boot_ms, target_system, target_component, coordinate_frame, type_mask, x, y, z, vx, vy, vz, afx, afy, afz, yaw, yaw_rate))

        def position_target_local_ned_encode(self, time_boot_ms, coordinate_frame, type_mask, x, y, z, vx, vy, vz, afx, afy, afz, yaw, yaw_rate):
                '''
                Set vehicle position, velocity and acceleration setpoint in local
                frame.

                time_boot_ms              : Timestamp in milliseconds since system boot (uint32_t)
                coordinate_frame          : Valid options are: MAV_FRAME_LOCAL_NED = 1, MAV_FRAME_LOCAL_OFFSET_NED = 7, MAV_FRAME_BODY_NED = 8, MAV_FRAME_BODY_OFFSET_NED = 9 (uint8_t)
                type_mask                 : Bitmask to indicate which dimensions should be ignored by the vehicle: a value of 0b0000000000000000 or 0b0000001000000000 indicates that none of the setpoint dimensions should be ignored. If bit 10 is set the floats afx afy afz should be interpreted as force instead of acceleration. Mapping: bit 1: x, bit 2: y, bit 3: z, bit 4: vx, bit 5: vy, bit 6: vz, bit 7: ax, bit 8: ay, bit 9: az, bit 10: is force setpoint, bit 11: yaw, bit 12: yaw rate (uint16_t)
                x                         : X Position in NED frame in meters (float)
                y                         : Y Position in NED frame in meters (float)
                z                         : Z Position in NED frame in meters (note, altitude is negative in NED) (float)
                vx                        : X velocity in NED frame in meter / s (float)
                vy                        : Y velocity in NED frame in meter / s (float)
                vz                        : Z velocity in NED frame in meter / s (float)
                afx                       : X acceleration or force (if bit 10 of type_mask is set) in NED frame in meter / s^2 or N (float)
                afy                       : Y acceleration or force (if bit 10 of type_mask is set) in NED frame in meter / s^2 or N (float)
                afz                       : Z acceleration or force (if bit 10 of type_mask is set) in NED frame in meter / s^2 or N (float)
                yaw                       : yaw setpoint in rad (float)
                yaw_rate                  : yaw rate setpoint in rad/s (float)

                '''
                return MAVLink_position_target_local_ned_message(time_boot_ms, coordinate_frame, type_mask, x, y, z, vx, vy, vz, afx, afy, afz, yaw, yaw_rate)

        def position_target_local_ned_send(self, time_boot_ms, coordinate_frame, type_mask, x, y, z, vx, vy, vz, afx, afy, afz, yaw, yaw_rate):
                '''
                Set vehicle position, velocity and acceleration setpoint in local
                frame.

                time_boot_ms              : Timestamp in milliseconds since system boot (uint32_t)
                coordinate_frame          : Valid options are: MAV_FRAME_LOCAL_NED = 1, MAV_FRAME_LOCAL_OFFSET_NED = 7, MAV_FRAME_BODY_NED = 8, MAV_FRAME_BODY_OFFSET_NED = 9 (uint8_t)
                type_mask                 : Bitmask to indicate which dimensions should be ignored by the vehicle: a value of 0b0000000000000000 or 0b0000001000000000 indicates that none of the setpoint dimensions should be ignored. If bit 10 is set the floats afx afy afz should be interpreted as force instead of acceleration. Mapping: bit 1: x, bit 2: y, bit 3: z, bit 4: vx, bit 5: vy, bit 6: vz, bit 7: ax, bit 8: ay, bit 9: az, bit 10: is force setpoint, bit 11: yaw, bit 12: yaw rate (uint16_t)
                x                         : X Position in NED frame in meters (float)
                y                         : Y Position in NED frame in meters (float)
                z                         : Z Position in NED frame in meters (note, altitude is negative in NED) (float)
                vx                        : X velocity in NED frame in meter / s (float)
                vy                        : Y velocity in NED frame in meter / s (float)
                vz                        : Z velocity in NED frame in meter / s (float)
                afx                       : X acceleration or force (if bit 10 of type_mask is set) in NED frame in meter / s^2 or N (float)
                afy                       : Y acceleration or force (if bit 10 of type_mask is set) in NED frame in meter / s^2 or N (float)
                afz                       : Z acceleration or force (if bit 10 of type_mask is set) in NED frame in meter / s^2 or N (float)
                yaw                       : yaw setpoint in rad (float)
                yaw_rate                  : yaw rate setpoint in rad/s (float)

                '''
                return self.send(self.position_target_local_ned_encode(time_boot_ms, coordinate_frame, type_mask, x, y, z, vx, vy, vz, afx, afy, afz, yaw, yaw_rate))

        def set_position_target_global_int_encode(self, time_boot_ms, target_system, target_component, coordinate_frame, type_mask, lat_int, lon_int, alt, vx, vy, vz, afx, afy, afz, yaw, yaw_rate):
                '''
                Set vehicle position, velocity and acceleration setpoint in the WGS84
                coordinate system.

                time_boot_ms              : Timestamp in milliseconds since system boot. The rationale for the timestamp in the setpoint is to allow the system to compensate for the transport delay of the setpoint. This allows the system to compensate processing latency. (uint32_t)
                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                coordinate_frame          : Valid options are: MAV_FRAME_GLOBAL_INT = 5, MAV_FRAME_GLOBAL_RELATIVE_ALT_INT = 6, MAV_FRAME_GLOBAL_TERRAIN_ALT_INT = 11 (uint8_t)
                type_mask                 : Bitmask to indicate which dimensions should be ignored by the vehicle: a value of 0b0000000000000000 or 0b0000001000000000 indicates that none of the setpoint dimensions should be ignored. If bit 10 is set the floats afx afy afz should be interpreted as force instead of acceleration. Mapping: bit 1: x, bit 2: y, bit 3: z, bit 4: vx, bit 5: vy, bit 6: vz, bit 7: ax, bit 8: ay, bit 9: az, bit 10: is force setpoint, bit 11: yaw, bit 12: yaw rate (uint16_t)
                lat_int                   : X Position in WGS84 frame in 1e7 * meters (int32_t)
                lon_int                   : Y Position in WGS84 frame in 1e7 * meters (int32_t)
                alt                       : Altitude in meters in AMSL altitude, not WGS84 if absolute or relative, above terrain if GLOBAL_TERRAIN_ALT_INT (float)
                vx                        : X velocity in NED frame in meter / s (float)
                vy                        : Y velocity in NED frame in meter / s (float)
                vz                        : Z velocity in NED frame in meter / s (float)
                afx                       : X acceleration or force (if bit 10 of type_mask is set) in NED frame in meter / s^2 or N (float)
                afy                       : Y acceleration or force (if bit 10 of type_mask is set) in NED frame in meter / s^2 or N (float)
                afz                       : Z acceleration or force (if bit 10 of type_mask is set) in NED frame in meter / s^2 or N (float)
                yaw                       : yaw setpoint in rad (float)
                yaw_rate                  : yaw rate setpoint in rad/s (float)

                '''
                return MAVLink_set_position_target_global_int_message(time_boot_ms, target_system, target_component, coordinate_frame, type_mask, lat_int, lon_int, alt, vx, vy, vz, afx, afy, afz, yaw, yaw_rate)

        def set_position_target_global_int_send(self, time_boot_ms, target_system, target_component, coordinate_frame, type_mask, lat_int, lon_int, alt, vx, vy, vz, afx, afy, afz, yaw, yaw_rate):
                '''
                Set vehicle position, velocity and acceleration setpoint in the WGS84
                coordinate system.

                time_boot_ms              : Timestamp in milliseconds since system boot. The rationale for the timestamp in the setpoint is to allow the system to compensate for the transport delay of the setpoint. This allows the system to compensate processing latency. (uint32_t)
                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                coordinate_frame          : Valid options are: MAV_FRAME_GLOBAL_INT = 5, MAV_FRAME_GLOBAL_RELATIVE_ALT_INT = 6, MAV_FRAME_GLOBAL_TERRAIN_ALT_INT = 11 (uint8_t)
                type_mask                 : Bitmask to indicate which dimensions should be ignored by the vehicle: a value of 0b0000000000000000 or 0b0000001000000000 indicates that none of the setpoint dimensions should be ignored. If bit 10 is set the floats afx afy afz should be interpreted as force instead of acceleration. Mapping: bit 1: x, bit 2: y, bit 3: z, bit 4: vx, bit 5: vy, bit 6: vz, bit 7: ax, bit 8: ay, bit 9: az, bit 10: is force setpoint, bit 11: yaw, bit 12: yaw rate (uint16_t)
                lat_int                   : X Position in WGS84 frame in 1e7 * meters (int32_t)
                lon_int                   : Y Position in WGS84 frame in 1e7 * meters (int32_t)
                alt                       : Altitude in meters in AMSL altitude, not WGS84 if absolute or relative, above terrain if GLOBAL_TERRAIN_ALT_INT (float)
                vx                        : X velocity in NED frame in meter / s (float)
                vy                        : Y velocity in NED frame in meter / s (float)
                vz                        : Z velocity in NED frame in meter / s (float)
                afx                       : X acceleration or force (if bit 10 of type_mask is set) in NED frame in meter / s^2 or N (float)
                afy                       : Y acceleration or force (if bit 10 of type_mask is set) in NED frame in meter / s^2 or N (float)
                afz                       : Z acceleration or force (if bit 10 of type_mask is set) in NED frame in meter / s^2 or N (float)
                yaw                       : yaw setpoint in rad (float)
                yaw_rate                  : yaw rate setpoint in rad/s (float)

                '''
                return self.send(self.set_position_target_global_int_encode(time_boot_ms, target_system, target_component, coordinate_frame, type_mask, lat_int, lon_int, alt, vx, vy, vz, afx, afy, afz, yaw, yaw_rate))

        def position_target_global_int_encode(self, time_boot_ms, coordinate_frame, type_mask, lat_int, lon_int, alt, vx, vy, vz, afx, afy, afz, yaw, yaw_rate):
                '''
                Set vehicle position, velocity and acceleration setpoint in the WGS84
                coordinate system.

                time_boot_ms              : Timestamp in milliseconds since system boot. The rationale for the timestamp in the setpoint is to allow the system to compensate for the transport delay of the setpoint. This allows the system to compensate processing latency. (uint32_t)
                coordinate_frame          : Valid options are: MAV_FRAME_GLOBAL_INT = 5, MAV_FRAME_GLOBAL_RELATIVE_ALT_INT = 6, MAV_FRAME_GLOBAL_TERRAIN_ALT_INT = 11 (uint8_t)
                type_mask                 : Bitmask to indicate which dimensions should be ignored by the vehicle: a value of 0b0000000000000000 or 0b0000001000000000 indicates that none of the setpoint dimensions should be ignored. If bit 10 is set the floats afx afy afz should be interpreted as force instead of acceleration. Mapping: bit 1: x, bit 2: y, bit 3: z, bit 4: vx, bit 5: vy, bit 6: vz, bit 7: ax, bit 8: ay, bit 9: az, bit 10: is force setpoint, bit 11: yaw, bit 12: yaw rate (uint16_t)
                lat_int                   : X Position in WGS84 frame in 1e7 * meters (int32_t)
                lon_int                   : Y Position in WGS84 frame in 1e7 * meters (int32_t)
                alt                       : Altitude in meters in AMSL altitude, not WGS84 if absolute or relative, above terrain if GLOBAL_TERRAIN_ALT_INT (float)
                vx                        : X velocity in NED frame in meter / s (float)
                vy                        : Y velocity in NED frame in meter / s (float)
                vz                        : Z velocity in NED frame in meter / s (float)
                afx                       : X acceleration or force (if bit 10 of type_mask is set) in NED frame in meter / s^2 or N (float)
                afy                       : Y acceleration or force (if bit 10 of type_mask is set) in NED frame in meter / s^2 or N (float)
                afz                       : Z acceleration or force (if bit 10 of type_mask is set) in NED frame in meter / s^2 or N (float)
                yaw                       : yaw setpoint in rad (float)
                yaw_rate                  : yaw rate setpoint in rad/s (float)

                '''
                return MAVLink_position_target_global_int_message(time_boot_ms, coordinate_frame, type_mask, lat_int, lon_int, alt, vx, vy, vz, afx, afy, afz, yaw, yaw_rate)

        def position_target_global_int_send(self, time_boot_ms, coordinate_frame, type_mask, lat_int, lon_int, alt, vx, vy, vz, afx, afy, afz, yaw, yaw_rate):
                '''
                Set vehicle position, velocity and acceleration setpoint in the WGS84
                coordinate system.

                time_boot_ms              : Timestamp in milliseconds since system boot. The rationale for the timestamp in the setpoint is to allow the system to compensate for the transport delay of the setpoint. This allows the system to compensate processing latency. (uint32_t)
                coordinate_frame          : Valid options are: MAV_FRAME_GLOBAL_INT = 5, MAV_FRAME_GLOBAL_RELATIVE_ALT_INT = 6, MAV_FRAME_GLOBAL_TERRAIN_ALT_INT = 11 (uint8_t)
                type_mask                 : Bitmask to indicate which dimensions should be ignored by the vehicle: a value of 0b0000000000000000 or 0b0000001000000000 indicates that none of the setpoint dimensions should be ignored. If bit 10 is set the floats afx afy afz should be interpreted as force instead of acceleration. Mapping: bit 1: x, bit 2: y, bit 3: z, bit 4: vx, bit 5: vy, bit 6: vz, bit 7: ax, bit 8: ay, bit 9: az, bit 10: is force setpoint, bit 11: yaw, bit 12: yaw rate (uint16_t)
                lat_int                   : X Position in WGS84 frame in 1e7 * meters (int32_t)
                lon_int                   : Y Position in WGS84 frame in 1e7 * meters (int32_t)
                alt                       : Altitude in meters in AMSL altitude, not WGS84 if absolute or relative, above terrain if GLOBAL_TERRAIN_ALT_INT (float)
                vx                        : X velocity in NED frame in meter / s (float)
                vy                        : Y velocity in NED frame in meter / s (float)
                vz                        : Z velocity in NED frame in meter / s (float)
                afx                       : X acceleration or force (if bit 10 of type_mask is set) in NED frame in meter / s^2 or N (float)
                afy                       : Y acceleration or force (if bit 10 of type_mask is set) in NED frame in meter / s^2 or N (float)
                afz                       : Z acceleration or force (if bit 10 of type_mask is set) in NED frame in meter / s^2 or N (float)
                yaw                       : yaw setpoint in rad (float)
                yaw_rate                  : yaw rate setpoint in rad/s (float)

                '''
                return self.send(self.position_target_global_int_encode(time_boot_ms, coordinate_frame, type_mask, lat_int, lon_int, alt, vx, vy, vz, afx, afy, afz, yaw, yaw_rate))

        def local_position_ned_system_global_offset_encode(self, time_boot_ms, x, y, z, roll, pitch, yaw):
                '''
                The offset in X, Y, Z and yaw between the LOCAL_POSITION_NED messages
                of MAV X and the global coordinate frame in NED
                coordinates. Coordinate frame is right-handed, Z-axis
                down (aeronautical frame, NED / north-east-down
                convention)

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                x                         : X Position (float)
                y                         : Y Position (float)
                z                         : Z Position (float)
                roll                      : Roll (float)
                pitch                     : Pitch (float)
                yaw                       : Yaw (float)

                '''
                return MAVLink_local_position_ned_system_global_offset_message(time_boot_ms, x, y, z, roll, pitch, yaw)

        def local_position_ned_system_global_offset_send(self, time_boot_ms, x, y, z, roll, pitch, yaw):
                '''
                The offset in X, Y, Z and yaw between the LOCAL_POSITION_NED messages
                of MAV X and the global coordinate frame in NED
                coordinates. Coordinate frame is right-handed, Z-axis
                down (aeronautical frame, NED / north-east-down
                convention)

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                x                         : X Position (float)
                y                         : Y Position (float)
                z                         : Z Position (float)
                roll                      : Roll (float)
                pitch                     : Pitch (float)
                yaw                       : Yaw (float)

                '''
                return self.send(self.local_position_ned_system_global_offset_encode(time_boot_ms, x, y, z, roll, pitch, yaw))

        def hil_state_encode(self, time_usec, roll, pitch, yaw, rollspeed, pitchspeed, yawspeed, lat, lon, alt, vx, vy, vz, xacc, yacc, zacc):
                '''
                DEPRECATED PACKET! Suffers from missing airspeed fields and
                singularities due to Euler angles. Please use
                HIL_STATE_QUATERNION instead. Sent from simulation to
                autopilot. This packet is useful for high throughput
                applications such as hardware in the loop simulations.

                time_usec                 : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
                roll                      : Roll angle (rad) (float)
                pitch                     : Pitch angle (rad) (float)
                yaw                       : Yaw angle (rad) (float)
                rollspeed                 : Body frame roll / phi angular speed (rad/s) (float)
                pitchspeed                : Body frame pitch / theta angular speed (rad/s) (float)
                yawspeed                  : Body frame yaw / psi angular speed (rad/s) (float)
                lat                       : Latitude, expressed as * 1E7 (int32_t)
                lon                       : Longitude, expressed as * 1E7 (int32_t)
                alt                       : Altitude in meters, expressed as * 1000 (millimeters) (int32_t)
                vx                        : Ground X Speed (Latitude), expressed as m/s * 100 (int16_t)
                vy                        : Ground Y Speed (Longitude), expressed as m/s * 100 (int16_t)
                vz                        : Ground Z Speed (Altitude), expressed as m/s * 100 (int16_t)
                xacc                      : X acceleration (mg) (int16_t)
                yacc                      : Y acceleration (mg) (int16_t)
                zacc                      : Z acceleration (mg) (int16_t)

                '''
                return MAVLink_hil_state_message(time_usec, roll, pitch, yaw, rollspeed, pitchspeed, yawspeed, lat, lon, alt, vx, vy, vz, xacc, yacc, zacc)

        def hil_state_send(self, time_usec, roll, pitch, yaw, rollspeed, pitchspeed, yawspeed, lat, lon, alt, vx, vy, vz, xacc, yacc, zacc):
                '''
                DEPRECATED PACKET! Suffers from missing airspeed fields and
                singularities due to Euler angles. Please use
                HIL_STATE_QUATERNION instead. Sent from simulation to
                autopilot. This packet is useful for high throughput
                applications such as hardware in the loop simulations.

                time_usec                 : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
                roll                      : Roll angle (rad) (float)
                pitch                     : Pitch angle (rad) (float)
                yaw                       : Yaw angle (rad) (float)
                rollspeed                 : Body frame roll / phi angular speed (rad/s) (float)
                pitchspeed                : Body frame pitch / theta angular speed (rad/s) (float)
                yawspeed                  : Body frame yaw / psi angular speed (rad/s) (float)
                lat                       : Latitude, expressed as * 1E7 (int32_t)
                lon                       : Longitude, expressed as * 1E7 (int32_t)
                alt                       : Altitude in meters, expressed as * 1000 (millimeters) (int32_t)
                vx                        : Ground X Speed (Latitude), expressed as m/s * 100 (int16_t)
                vy                        : Ground Y Speed (Longitude), expressed as m/s * 100 (int16_t)
                vz                        : Ground Z Speed (Altitude), expressed as m/s * 100 (int16_t)
                xacc                      : X acceleration (mg) (int16_t)
                yacc                      : Y acceleration (mg) (int16_t)
                zacc                      : Z acceleration (mg) (int16_t)

                '''
                return self.send(self.hil_state_encode(time_usec, roll, pitch, yaw, rollspeed, pitchspeed, yawspeed, lat, lon, alt, vx, vy, vz, xacc, yacc, zacc))

        def hil_controls_encode(self, time_usec, roll_ailerons, pitch_elevator, yaw_rudder, throttle, aux1, aux2, aux3, aux4, mode, nav_mode):
                '''
                Sent from autopilot to simulation. Hardware in the loop control
                outputs

                time_usec                 : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
                roll_ailerons             : Control output -1 .. 1 (float)
                pitch_elevator            : Control output -1 .. 1 (float)
                yaw_rudder                : Control output -1 .. 1 (float)
                throttle                  : Throttle 0 .. 1 (float)
                aux1                      : Aux 1, -1 .. 1 (float)
                aux2                      : Aux 2, -1 .. 1 (float)
                aux3                      : Aux 3, -1 .. 1 (float)
                aux4                      : Aux 4, -1 .. 1 (float)
                mode                      : System mode (MAV_MODE) (uint8_t)
                nav_mode                  : Navigation mode (MAV_NAV_MODE) (uint8_t)

                '''
                return MAVLink_hil_controls_message(time_usec, roll_ailerons, pitch_elevator, yaw_rudder, throttle, aux1, aux2, aux3, aux4, mode, nav_mode)

        def hil_controls_send(self, time_usec, roll_ailerons, pitch_elevator, yaw_rudder, throttle, aux1, aux2, aux3, aux4, mode, nav_mode):
                '''
                Sent from autopilot to simulation. Hardware in the loop control
                outputs

                time_usec                 : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
                roll_ailerons             : Control output -1 .. 1 (float)
                pitch_elevator            : Control output -1 .. 1 (float)
                yaw_rudder                : Control output -1 .. 1 (float)
                throttle                  : Throttle 0 .. 1 (float)
                aux1                      : Aux 1, -1 .. 1 (float)
                aux2                      : Aux 2, -1 .. 1 (float)
                aux3                      : Aux 3, -1 .. 1 (float)
                aux4                      : Aux 4, -1 .. 1 (float)
                mode                      : System mode (MAV_MODE) (uint8_t)
                nav_mode                  : Navigation mode (MAV_NAV_MODE) (uint8_t)

                '''
                return self.send(self.hil_controls_encode(time_usec, roll_ailerons, pitch_elevator, yaw_rudder, throttle, aux1, aux2, aux3, aux4, mode, nav_mode))

        def hil_rc_inputs_raw_encode(self, time_usec, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw, chan9_raw, chan10_raw, chan11_raw, chan12_raw, rssi):
                '''
                Sent from simulation to autopilot. The RAW values of the RC channels
                received. The standard PPM modulation is as follows:
                1000 microseconds: 0%, 2000 microseconds: 100%.
                Individual receivers/transmitters might violate this
                specification.

                time_usec                 : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
                chan1_raw                 : RC channel 1 value, in microseconds (uint16_t)
                chan2_raw                 : RC channel 2 value, in microseconds (uint16_t)
                chan3_raw                 : RC channel 3 value, in microseconds (uint16_t)
                chan4_raw                 : RC channel 4 value, in microseconds (uint16_t)
                chan5_raw                 : RC channel 5 value, in microseconds (uint16_t)
                chan6_raw                 : RC channel 6 value, in microseconds (uint16_t)
                chan7_raw                 : RC channel 7 value, in microseconds (uint16_t)
                chan8_raw                 : RC channel 8 value, in microseconds (uint16_t)
                chan9_raw                 : RC channel 9 value, in microseconds (uint16_t)
                chan10_raw                : RC channel 10 value, in microseconds (uint16_t)
                chan11_raw                : RC channel 11 value, in microseconds (uint16_t)
                chan12_raw                : RC channel 12 value, in microseconds (uint16_t)
                rssi                      : Receive signal strength indicator, 0: 0%, 255: 100% (uint8_t)

                '''
                return MAVLink_hil_rc_inputs_raw_message(time_usec, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw, chan9_raw, chan10_raw, chan11_raw, chan12_raw, rssi)

        def hil_rc_inputs_raw_send(self, time_usec, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw, chan9_raw, chan10_raw, chan11_raw, chan12_raw, rssi):
                '''
                Sent from simulation to autopilot. The RAW values of the RC channels
                received. The standard PPM modulation is as follows:
                1000 microseconds: 0%, 2000 microseconds: 100%.
                Individual receivers/transmitters might violate this
                specification.

                time_usec                 : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
                chan1_raw                 : RC channel 1 value, in microseconds (uint16_t)
                chan2_raw                 : RC channel 2 value, in microseconds (uint16_t)
                chan3_raw                 : RC channel 3 value, in microseconds (uint16_t)
                chan4_raw                 : RC channel 4 value, in microseconds (uint16_t)
                chan5_raw                 : RC channel 5 value, in microseconds (uint16_t)
                chan6_raw                 : RC channel 6 value, in microseconds (uint16_t)
                chan7_raw                 : RC channel 7 value, in microseconds (uint16_t)
                chan8_raw                 : RC channel 8 value, in microseconds (uint16_t)
                chan9_raw                 : RC channel 9 value, in microseconds (uint16_t)
                chan10_raw                : RC channel 10 value, in microseconds (uint16_t)
                chan11_raw                : RC channel 11 value, in microseconds (uint16_t)
                chan12_raw                : RC channel 12 value, in microseconds (uint16_t)
                rssi                      : Receive signal strength indicator, 0: 0%, 255: 100% (uint8_t)

                '''
                return self.send(self.hil_rc_inputs_raw_encode(time_usec, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw, chan9_raw, chan10_raw, chan11_raw, chan12_raw, rssi))

        def optical_flow_encode(self, time_usec, sensor_id, flow_x, flow_y, flow_comp_m_x, flow_comp_m_y, quality, ground_distance):
                '''
                Optical flow from a flow sensor (e.g. optical mouse sensor)

                time_usec                 : Timestamp (UNIX) (uint64_t)
                sensor_id                 : Sensor ID (uint8_t)
                flow_x                    : Flow in pixels * 10 in x-sensor direction (dezi-pixels) (int16_t)
                flow_y                    : Flow in pixels * 10 in y-sensor direction (dezi-pixels) (int16_t)
                flow_comp_m_x             : Flow in meters in x-sensor direction, angular-speed compensated (float)
                flow_comp_m_y             : Flow in meters in y-sensor direction, angular-speed compensated (float)
                quality                   : Optical flow quality / confidence. 0: bad, 255: maximum quality (uint8_t)
                ground_distance           : Ground distance in meters. Positive value: distance known. Negative value: Unknown distance (float)

                '''
                return MAVLink_optical_flow_message(time_usec, sensor_id, flow_x, flow_y, flow_comp_m_x, flow_comp_m_y, quality, ground_distance)

        def optical_flow_send(self, time_usec, sensor_id, flow_x, flow_y, flow_comp_m_x, flow_comp_m_y, quality, ground_distance):
                '''
                Optical flow from a flow sensor (e.g. optical mouse sensor)

                time_usec                 : Timestamp (UNIX) (uint64_t)
                sensor_id                 : Sensor ID (uint8_t)
                flow_x                    : Flow in pixels * 10 in x-sensor direction (dezi-pixels) (int16_t)
                flow_y                    : Flow in pixels * 10 in y-sensor direction (dezi-pixels) (int16_t)
                flow_comp_m_x             : Flow in meters in x-sensor direction, angular-speed compensated (float)
                flow_comp_m_y             : Flow in meters in y-sensor direction, angular-speed compensated (float)
                quality                   : Optical flow quality / confidence. 0: bad, 255: maximum quality (uint8_t)
                ground_distance           : Ground distance in meters. Positive value: distance known. Negative value: Unknown distance (float)

                '''
                return self.send(self.optical_flow_encode(time_usec, sensor_id, flow_x, flow_y, flow_comp_m_x, flow_comp_m_y, quality, ground_distance))

        def global_vision_position_estimate_encode(self, usec, x, y, z, roll, pitch, yaw):
                '''
                

                usec                      : Timestamp (microseconds, synced to UNIX time or since system boot) (uint64_t)
                x                         : Global X position (float)
                y                         : Global Y position (float)
                z                         : Global Z position (float)
                roll                      : Roll angle in rad (float)
                pitch                     : Pitch angle in rad (float)
                yaw                       : Yaw angle in rad (float)

                '''
                return MAVLink_global_vision_position_estimate_message(usec, x, y, z, roll, pitch, yaw)

        def global_vision_position_estimate_send(self, usec, x, y, z, roll, pitch, yaw):
                '''
                

                usec                      : Timestamp (microseconds, synced to UNIX time or since system boot) (uint64_t)
                x                         : Global X position (float)
                y                         : Global Y position (float)
                z                         : Global Z position (float)
                roll                      : Roll angle in rad (float)
                pitch                     : Pitch angle in rad (float)
                yaw                       : Yaw angle in rad (float)

                '''
                return self.send(self.global_vision_position_estimate_encode(usec, x, y, z, roll, pitch, yaw))

        def vision_position_estimate_encode(self, usec, x, y, z, roll, pitch, yaw):
                '''
                

                usec                      : Timestamp (microseconds, synced to UNIX time or since system boot) (uint64_t)
                x                         : Global X position (float)
                y                         : Global Y position (float)
                z                         : Global Z position (float)
                roll                      : Roll angle in rad (float)
                pitch                     : Pitch angle in rad (float)
                yaw                       : Yaw angle in rad (float)

                '''
                return MAVLink_vision_position_estimate_message(usec, x, y, z, roll, pitch, yaw)

        def vision_position_estimate_send(self, usec, x, y, z, roll, pitch, yaw):
                '''
                

                usec                      : Timestamp (microseconds, synced to UNIX time or since system boot) (uint64_t)
                x                         : Global X position (float)
                y                         : Global Y position (float)
                z                         : Global Z position (float)
                roll                      : Roll angle in rad (float)
                pitch                     : Pitch angle in rad (float)
                yaw                       : Yaw angle in rad (float)

                '''
                return self.send(self.vision_position_estimate_encode(usec, x, y, z, roll, pitch, yaw))

        def vision_speed_estimate_encode(self, usec, x, y, z):
                '''
                

                usec                      : Timestamp (microseconds, synced to UNIX time or since system boot) (uint64_t)
                x                         : Global X speed (float)
                y                         : Global Y speed (float)
                z                         : Global Z speed (float)

                '''
                return MAVLink_vision_speed_estimate_message(usec, x, y, z)

        def vision_speed_estimate_send(self, usec, x, y, z):
                '''
                

                usec                      : Timestamp (microseconds, synced to UNIX time or since system boot) (uint64_t)
                x                         : Global X speed (float)
                y                         : Global Y speed (float)
                z                         : Global Z speed (float)

                '''
                return self.send(self.vision_speed_estimate_encode(usec, x, y, z))

        def vicon_position_estimate_encode(self, usec, x, y, z, roll, pitch, yaw):
                '''
                

                usec                      : Timestamp (microseconds, synced to UNIX time or since system boot) (uint64_t)
                x                         : Global X position (float)
                y                         : Global Y position (float)
                z                         : Global Z position (float)
                roll                      : Roll angle in rad (float)
                pitch                     : Pitch angle in rad (float)
                yaw                       : Yaw angle in rad (float)

                '''
                return MAVLink_vicon_position_estimate_message(usec, x, y, z, roll, pitch, yaw)

        def vicon_position_estimate_send(self, usec, x, y, z, roll, pitch, yaw):
                '''
                

                usec                      : Timestamp (microseconds, synced to UNIX time or since system boot) (uint64_t)
                x                         : Global X position (float)
                y                         : Global Y position (float)
                z                         : Global Z position (float)
                roll                      : Roll angle in rad (float)
                pitch                     : Pitch angle in rad (float)
                yaw                       : Yaw angle in rad (float)

                '''
                return self.send(self.vicon_position_estimate_encode(usec, x, y, z, roll, pitch, yaw))

        def highres_imu_encode(self, time_usec, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag, abs_pressure, diff_pressure, pressure_alt, temperature, fields_updated):
                '''
                The IMU readings in SI units in NED body frame

                time_usec                 : Timestamp (microseconds, synced to UNIX time or since system boot) (uint64_t)
                xacc                      : X acceleration (m/s^2) (float)
                yacc                      : Y acceleration (m/s^2) (float)
                zacc                      : Z acceleration (m/s^2) (float)
                xgyro                     : Angular speed around X axis (rad / sec) (float)
                ygyro                     : Angular speed around Y axis (rad / sec) (float)
                zgyro                     : Angular speed around Z axis (rad / sec) (float)
                xmag                      : X Magnetic field (Gauss) (float)
                ymag                      : Y Magnetic field (Gauss) (float)
                zmag                      : Z Magnetic field (Gauss) (float)
                abs_pressure              : Absolute pressure in millibar (float)
                diff_pressure             : Differential pressure in millibar (float)
                pressure_alt              : Altitude calculated from pressure (float)
                temperature               : Temperature in degrees celsius (float)
                fields_updated            : Bitmask for fields that have updated since last message, bit 0 = xacc, bit 12: temperature (uint16_t)

                '''
                return MAVLink_highres_imu_message(time_usec, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag, abs_pressure, diff_pressure, pressure_alt, temperature, fields_updated)

        def highres_imu_send(self, time_usec, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag, abs_pressure, diff_pressure, pressure_alt, temperature, fields_updated):
                '''
                The IMU readings in SI units in NED body frame

                time_usec                 : Timestamp (microseconds, synced to UNIX time or since system boot) (uint64_t)
                xacc                      : X acceleration (m/s^2) (float)
                yacc                      : Y acceleration (m/s^2) (float)
                zacc                      : Z acceleration (m/s^2) (float)
                xgyro                     : Angular speed around X axis (rad / sec) (float)
                ygyro                     : Angular speed around Y axis (rad / sec) (float)
                zgyro                     : Angular speed around Z axis (rad / sec) (float)
                xmag                      : X Magnetic field (Gauss) (float)
                ymag                      : Y Magnetic field (Gauss) (float)
                zmag                      : Z Magnetic field (Gauss) (float)
                abs_pressure              : Absolute pressure in millibar (float)
                diff_pressure             : Differential pressure in millibar (float)
                pressure_alt              : Altitude calculated from pressure (float)
                temperature               : Temperature in degrees celsius (float)
                fields_updated            : Bitmask for fields that have updated since last message, bit 0 = xacc, bit 12: temperature (uint16_t)

                '''
                return self.send(self.highres_imu_encode(time_usec, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag, abs_pressure, diff_pressure, pressure_alt, temperature, fields_updated))

        def optical_flow_rad_encode(self, time_usec, sensor_id, integration_time_us, integrated_x, integrated_y, integrated_xgyro, integrated_ygyro, integrated_zgyro, temperature, quality, time_delta_distance_us, distance):
                '''
                Optical flow from an angular rate flow sensor (e.g. PX4FLOW or mouse
                sensor)

                time_usec                 : Timestamp (microseconds, synced to UNIX time or since system boot) (uint64_t)
                sensor_id                 : Sensor ID (uint8_t)
                integration_time_us        : Integration time in microseconds. Divide integrated_x and integrated_y by the integration time to obtain average flow. The integration time also indicates the. (uint32_t)
                integrated_x              : Flow in radians around X axis (Sensor RH rotation about the X axis induces a positive flow. Sensor linear motion along the positive Y axis induces a negative flow.) (float)
                integrated_y              : Flow in radians around Y axis (Sensor RH rotation about the Y axis induces a positive flow. Sensor linear motion along the positive X axis induces a positive flow.) (float)
                integrated_xgyro          : RH rotation around X axis (rad) (float)
                integrated_ygyro          : RH rotation around Y axis (rad) (float)
                integrated_zgyro          : RH rotation around Z axis (rad) (float)
                temperature               : Temperature * 100 in centi-degrees Celsius (int16_t)
                quality                   : Optical flow quality / confidence. 0: no valid flow, 255: maximum quality (uint8_t)
                time_delta_distance_us        : Time in microseconds since the distance was sampled. (uint32_t)
                distance                  : Distance to the center of the flow field in meters. Positive value (including zero): distance known. Negative value: Unknown distance. (float)

                '''
                return MAVLink_optical_flow_rad_message(time_usec, sensor_id, integration_time_us, integrated_x, integrated_y, integrated_xgyro, integrated_ygyro, integrated_zgyro, temperature, quality, time_delta_distance_us, distance)

        def optical_flow_rad_send(self, time_usec, sensor_id, integration_time_us, integrated_x, integrated_y, integrated_xgyro, integrated_ygyro, integrated_zgyro, temperature, quality, time_delta_distance_us, distance):
                '''
                Optical flow from an angular rate flow sensor (e.g. PX4FLOW or mouse
                sensor)

                time_usec                 : Timestamp (microseconds, synced to UNIX time or since system boot) (uint64_t)
                sensor_id                 : Sensor ID (uint8_t)
                integration_time_us        : Integration time in microseconds. Divide integrated_x and integrated_y by the integration time to obtain average flow. The integration time also indicates the. (uint32_t)
                integrated_x              : Flow in radians around X axis (Sensor RH rotation about the X axis induces a positive flow. Sensor linear motion along the positive Y axis induces a negative flow.) (float)
                integrated_y              : Flow in radians around Y axis (Sensor RH rotation about the Y axis induces a positive flow. Sensor linear motion along the positive X axis induces a positive flow.) (float)
                integrated_xgyro          : RH rotation around X axis (rad) (float)
                integrated_ygyro          : RH rotation around Y axis (rad) (float)
                integrated_zgyro          : RH rotation around Z axis (rad) (float)
                temperature               : Temperature * 100 in centi-degrees Celsius (int16_t)
                quality                   : Optical flow quality / confidence. 0: no valid flow, 255: maximum quality (uint8_t)
                time_delta_distance_us        : Time in microseconds since the distance was sampled. (uint32_t)
                distance                  : Distance to the center of the flow field in meters. Positive value (including zero): distance known. Negative value: Unknown distance. (float)

                '''
                return self.send(self.optical_flow_rad_encode(time_usec, sensor_id, integration_time_us, integrated_x, integrated_y, integrated_xgyro, integrated_ygyro, integrated_zgyro, temperature, quality, time_delta_distance_us, distance))

        def hil_sensor_encode(self, time_usec, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag, abs_pressure, diff_pressure, pressure_alt, temperature, fields_updated):
                '''
                The IMU readings in SI units in NED body frame

                time_usec                 : Timestamp (microseconds, synced to UNIX time or since system boot) (uint64_t)
                xacc                      : X acceleration (m/s^2) (float)
                yacc                      : Y acceleration (m/s^2) (float)
                zacc                      : Z acceleration (m/s^2) (float)
                xgyro                     : Angular speed around X axis in body frame (rad / sec) (float)
                ygyro                     : Angular speed around Y axis in body frame (rad / sec) (float)
                zgyro                     : Angular speed around Z axis in body frame (rad / sec) (float)
                xmag                      : X Magnetic field (Gauss) (float)
                ymag                      : Y Magnetic field (Gauss) (float)
                zmag                      : Z Magnetic field (Gauss) (float)
                abs_pressure              : Absolute pressure in millibar (float)
                diff_pressure             : Differential pressure (airspeed) in millibar (float)
                pressure_alt              : Altitude calculated from pressure (float)
                temperature               : Temperature in degrees celsius (float)
                fields_updated            : Bitmask for fields that have updated since last message, bit 0 = xacc, bit 12: temperature (uint32_t)

                '''
                return MAVLink_hil_sensor_message(time_usec, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag, abs_pressure, diff_pressure, pressure_alt, temperature, fields_updated)

        def hil_sensor_send(self, time_usec, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag, abs_pressure, diff_pressure, pressure_alt, temperature, fields_updated):
                '''
                The IMU readings in SI units in NED body frame

                time_usec                 : Timestamp (microseconds, synced to UNIX time or since system boot) (uint64_t)
                xacc                      : X acceleration (m/s^2) (float)
                yacc                      : Y acceleration (m/s^2) (float)
                zacc                      : Z acceleration (m/s^2) (float)
                xgyro                     : Angular speed around X axis in body frame (rad / sec) (float)
                ygyro                     : Angular speed around Y axis in body frame (rad / sec) (float)
                zgyro                     : Angular speed around Z axis in body frame (rad / sec) (float)
                xmag                      : X Magnetic field (Gauss) (float)
                ymag                      : Y Magnetic field (Gauss) (float)
                zmag                      : Z Magnetic field (Gauss) (float)
                abs_pressure              : Absolute pressure in millibar (float)
                diff_pressure             : Differential pressure (airspeed) in millibar (float)
                pressure_alt              : Altitude calculated from pressure (float)
                temperature               : Temperature in degrees celsius (float)
                fields_updated            : Bitmask for fields that have updated since last message, bit 0 = xacc, bit 12: temperature (uint32_t)

                '''
                return self.send(self.hil_sensor_encode(time_usec, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag, abs_pressure, diff_pressure, pressure_alt, temperature, fields_updated))

        def sim_state_encode(self, q1, q2, q3, q4, roll, pitch, yaw, xacc, yacc, zacc, xgyro, ygyro, zgyro, lat, lon, alt, std_dev_horz, std_dev_vert, vn, ve, vd):
                '''
                Status of simulation environment, if used

                q1                        : True attitude quaternion component 1, w (1 in null-rotation) (float)
                q2                        : True attitude quaternion component 2, x (0 in null-rotation) (float)
                q3                        : True attitude quaternion component 3, y (0 in null-rotation) (float)
                q4                        : True attitude quaternion component 4, z (0 in null-rotation) (float)
                roll                      : Attitude roll expressed as Euler angles, not recommended except for human-readable outputs (float)
                pitch                     : Attitude pitch expressed as Euler angles, not recommended except for human-readable outputs (float)
                yaw                       : Attitude yaw expressed as Euler angles, not recommended except for human-readable outputs (float)
                xacc                      : X acceleration m/s/s (float)
                yacc                      : Y acceleration m/s/s (float)
                zacc                      : Z acceleration m/s/s (float)
                xgyro                     : Angular speed around X axis rad/s (float)
                ygyro                     : Angular speed around Y axis rad/s (float)
                zgyro                     : Angular speed around Z axis rad/s (float)
                lat                       : Latitude in degrees (float)
                lon                       : Longitude in degrees (float)
                alt                       : Altitude in meters (float)
                std_dev_horz              : Horizontal position standard deviation (float)
                std_dev_vert              : Vertical position standard deviation (float)
                vn                        : True velocity in m/s in NORTH direction in earth-fixed NED frame (float)
                ve                        : True velocity in m/s in EAST direction in earth-fixed NED frame (float)
                vd                        : True velocity in m/s in DOWN direction in earth-fixed NED frame (float)

                '''
                return MAVLink_sim_state_message(q1, q2, q3, q4, roll, pitch, yaw, xacc, yacc, zacc, xgyro, ygyro, zgyro, lat, lon, alt, std_dev_horz, std_dev_vert, vn, ve, vd)

        def sim_state_send(self, q1, q2, q3, q4, roll, pitch, yaw, xacc, yacc, zacc, xgyro, ygyro, zgyro, lat, lon, alt, std_dev_horz, std_dev_vert, vn, ve, vd):
                '''
                Status of simulation environment, if used

                q1                        : True attitude quaternion component 1, w (1 in null-rotation) (float)
                q2                        : True attitude quaternion component 2, x (0 in null-rotation) (float)
                q3                        : True attitude quaternion component 3, y (0 in null-rotation) (float)
                q4                        : True attitude quaternion component 4, z (0 in null-rotation) (float)
                roll                      : Attitude roll expressed as Euler angles, not recommended except for human-readable outputs (float)
                pitch                     : Attitude pitch expressed as Euler angles, not recommended except for human-readable outputs (float)
                yaw                       : Attitude yaw expressed as Euler angles, not recommended except for human-readable outputs (float)
                xacc                      : X acceleration m/s/s (float)
                yacc                      : Y acceleration m/s/s (float)
                zacc                      : Z acceleration m/s/s (float)
                xgyro                     : Angular speed around X axis rad/s (float)
                ygyro                     : Angular speed around Y axis rad/s (float)
                zgyro                     : Angular speed around Z axis rad/s (float)
                lat                       : Latitude in degrees (float)
                lon                       : Longitude in degrees (float)
                alt                       : Altitude in meters (float)
                std_dev_horz              : Horizontal position standard deviation (float)
                std_dev_vert              : Vertical position standard deviation (float)
                vn                        : True velocity in m/s in NORTH direction in earth-fixed NED frame (float)
                ve                        : True velocity in m/s in EAST direction in earth-fixed NED frame (float)
                vd                        : True velocity in m/s in DOWN direction in earth-fixed NED frame (float)

                '''
                return self.send(self.sim_state_encode(q1, q2, q3, q4, roll, pitch, yaw, xacc, yacc, zacc, xgyro, ygyro, zgyro, lat, lon, alt, std_dev_horz, std_dev_vert, vn, ve, vd))

        def radio_status_encode(self, rssi, remrssi, txbuf, noise, remnoise, rxerrors, fixed):
                '''
                Status generated by radio and injected into MAVLink stream.

                rssi                      : Local signal strength (uint8_t)
                remrssi                   : Remote signal strength (uint8_t)
                txbuf                     : Remaining free buffer space in percent. (uint8_t)
                noise                     : Background noise level (uint8_t)
                remnoise                  : Remote background noise level (uint8_t)
                rxerrors                  : Receive errors (uint16_t)
                fixed                     : Count of error corrected packets (uint16_t)

                '''
                return MAVLink_radio_status_message(rssi, remrssi, txbuf, noise, remnoise, rxerrors, fixed)

        def radio_status_send(self, rssi, remrssi, txbuf, noise, remnoise, rxerrors, fixed):
                '''
                Status generated by radio and injected into MAVLink stream.

                rssi                      : Local signal strength (uint8_t)
                remrssi                   : Remote signal strength (uint8_t)
                txbuf                     : Remaining free buffer space in percent. (uint8_t)
                noise                     : Background noise level (uint8_t)
                remnoise                  : Remote background noise level (uint8_t)
                rxerrors                  : Receive errors (uint16_t)
                fixed                     : Count of error corrected packets (uint16_t)

                '''
                return self.send(self.radio_status_encode(rssi, remrssi, txbuf, noise, remnoise, rxerrors, fixed))

        def file_transfer_protocol_encode(self, target_network, target_system, target_component, payload):
                '''
                File transfer message

                target_network            : Network ID (0 for broadcast) (uint8_t)
                target_system             : System ID (0 for broadcast) (uint8_t)
                target_component          : Component ID (0 for broadcast) (uint8_t)
                payload                   : Variable length payload. The length is defined by the remaining message length when subtracting the header and other fields.  The entire content of this block is opaque unless you understand any the encoding message_type.  The particular encoding used can be extension specific and might not always be documented as part of the mavlink specification. (uint8_t)

                '''
                return MAVLink_file_transfer_protocol_message(target_network, target_system, target_component, payload)

        def file_transfer_protocol_send(self, target_network, target_system, target_component, payload):
                '''
                File transfer message

                target_network            : Network ID (0 for broadcast) (uint8_t)
                target_system             : System ID (0 for broadcast) (uint8_t)
                target_component          : Component ID (0 for broadcast) (uint8_t)
                payload                   : Variable length payload. The length is defined by the remaining message length when subtracting the header and other fields.  The entire content of this block is opaque unless you understand any the encoding message_type.  The particular encoding used can be extension specific and might not always be documented as part of the mavlink specification. (uint8_t)

                '''
                return self.send(self.file_transfer_protocol_encode(target_network, target_system, target_component, payload))

        def timesync_encode(self, tc1, ts1):
                '''
                Time synchronization message.

                tc1                       : Time sync timestamp 1 (int64_t)
                ts1                       : Time sync timestamp 2 (int64_t)

                '''
                return MAVLink_timesync_message(tc1, ts1)

        def timesync_send(self, tc1, ts1):
                '''
                Time synchronization message.

                tc1                       : Time sync timestamp 1 (int64_t)
                ts1                       : Time sync timestamp 2 (int64_t)

                '''
                return self.send(self.timesync_encode(tc1, ts1))

        def camera_trigger_encode(self, time_usec, seq):
                '''
                Camera-IMU triggering and synchronisation message.

                time_usec                 : Timestamp for the image frame in microseconds (uint64_t)
                seq                       : Image frame sequence (uint32_t)

                '''
                return MAVLink_camera_trigger_message(time_usec, seq)

        def camera_trigger_send(self, time_usec, seq):
                '''
                Camera-IMU triggering and synchronisation message.

                time_usec                 : Timestamp for the image frame in microseconds (uint64_t)
                seq                       : Image frame sequence (uint32_t)

                '''
                return self.send(self.camera_trigger_encode(time_usec, seq))

        def hil_gps_encode(self, time_usec, fix_type, lat, lon, alt, eph, epv, vel, vn, ve, vd, cog, satellites_visible):
                '''
                The global position, as returned by the Global Positioning System
                (GPS). This is                  NOT the global
                position estimate of the sytem, but rather a RAW
                sensor value. See message GLOBAL_POSITION for the
                global position estimate. Coordinate frame is right-
                handed, Z-axis up (GPS frame).

                time_usec                 : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
                fix_type                  : 0-1: no fix, 2: 2D fix, 3: 3D fix. Some applications will not use the value of this field unless it is at least two, so always correctly fill in the fix. (uint8_t)
                lat                       : Latitude (WGS84), in degrees * 1E7 (int32_t)
                lon                       : Longitude (WGS84), in degrees * 1E7 (int32_t)
                alt                       : Altitude (AMSL, not WGS84), in meters * 1000 (positive for up) (int32_t)
                eph                       : GPS HDOP horizontal dilution of position in cm (m*100). If unknown, set to: 65535 (uint16_t)
                epv                       : GPS VDOP vertical dilution of position in cm (m*100). If unknown, set to: 65535 (uint16_t)
                vel                       : GPS ground speed (m/s * 100). If unknown, set to: 65535 (uint16_t)
                vn                        : GPS velocity in cm/s in NORTH direction in earth-fixed NED frame (int16_t)
                ve                        : GPS velocity in cm/s in EAST direction in earth-fixed NED frame (int16_t)
                vd                        : GPS velocity in cm/s in DOWN direction in earth-fixed NED frame (int16_t)
                cog                       : Course over ground (NOT heading, but direction of movement) in degrees * 100, 0.0..359.99 degrees. If unknown, set to: 65535 (uint16_t)
                satellites_visible        : Number of satellites visible. If unknown, set to 255 (uint8_t)

                '''
                return MAVLink_hil_gps_message(time_usec, fix_type, lat, lon, alt, eph, epv, vel, vn, ve, vd, cog, satellites_visible)

        def hil_gps_send(self, time_usec, fix_type, lat, lon, alt, eph, epv, vel, vn, ve, vd, cog, satellites_visible):
                '''
                The global position, as returned by the Global Positioning System
                (GPS). This is                  NOT the global
                position estimate of the sytem, but rather a RAW
                sensor value. See message GLOBAL_POSITION for the
                global position estimate. Coordinate frame is right-
                handed, Z-axis up (GPS frame).

                time_usec                 : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
                fix_type                  : 0-1: no fix, 2: 2D fix, 3: 3D fix. Some applications will not use the value of this field unless it is at least two, so always correctly fill in the fix. (uint8_t)
                lat                       : Latitude (WGS84), in degrees * 1E7 (int32_t)
                lon                       : Longitude (WGS84), in degrees * 1E7 (int32_t)
                alt                       : Altitude (AMSL, not WGS84), in meters * 1000 (positive for up) (int32_t)
                eph                       : GPS HDOP horizontal dilution of position in cm (m*100). If unknown, set to: 65535 (uint16_t)
                epv                       : GPS VDOP vertical dilution of position in cm (m*100). If unknown, set to: 65535 (uint16_t)
                vel                       : GPS ground speed (m/s * 100). If unknown, set to: 65535 (uint16_t)
                vn                        : GPS velocity in cm/s in NORTH direction in earth-fixed NED frame (int16_t)
                ve                        : GPS velocity in cm/s in EAST direction in earth-fixed NED frame (int16_t)
                vd                        : GPS velocity in cm/s in DOWN direction in earth-fixed NED frame (int16_t)
                cog                       : Course over ground (NOT heading, but direction of movement) in degrees * 100, 0.0..359.99 degrees. If unknown, set to: 65535 (uint16_t)
                satellites_visible        : Number of satellites visible. If unknown, set to 255 (uint8_t)

                '''
                return self.send(self.hil_gps_encode(time_usec, fix_type, lat, lon, alt, eph, epv, vel, vn, ve, vd, cog, satellites_visible))

        def hil_optical_flow_encode(self, time_usec, sensor_id, integration_time_us, integrated_x, integrated_y, integrated_xgyro, integrated_ygyro, integrated_zgyro, temperature, quality, time_delta_distance_us, distance):
                '''
                Simulated optical flow from a flow sensor (e.g. PX4FLOW or optical
                mouse sensor)

                time_usec                 : Timestamp (microseconds, synced to UNIX time or since system boot) (uint64_t)
                sensor_id                 : Sensor ID (uint8_t)
                integration_time_us        : Integration time in microseconds. Divide integrated_x and integrated_y by the integration time to obtain average flow. The integration time also indicates the. (uint32_t)
                integrated_x              : Flow in radians around X axis (Sensor RH rotation about the X axis induces a positive flow. Sensor linear motion along the positive Y axis induces a negative flow.) (float)
                integrated_y              : Flow in radians around Y axis (Sensor RH rotation about the Y axis induces a positive flow. Sensor linear motion along the positive X axis induces a positive flow.) (float)
                integrated_xgyro          : RH rotation around X axis (rad) (float)
                integrated_ygyro          : RH rotation around Y axis (rad) (float)
                integrated_zgyro          : RH rotation around Z axis (rad) (float)
                temperature               : Temperature * 100 in centi-degrees Celsius (int16_t)
                quality                   : Optical flow quality / confidence. 0: no valid flow, 255: maximum quality (uint8_t)
                time_delta_distance_us        : Time in microseconds since the distance was sampled. (uint32_t)
                distance                  : Distance to the center of the flow field in meters. Positive value (including zero): distance known. Negative value: Unknown distance. (float)

                '''
                return MAVLink_hil_optical_flow_message(time_usec, sensor_id, integration_time_us, integrated_x, integrated_y, integrated_xgyro, integrated_ygyro, integrated_zgyro, temperature, quality, time_delta_distance_us, distance)

        def hil_optical_flow_send(self, time_usec, sensor_id, integration_time_us, integrated_x, integrated_y, integrated_xgyro, integrated_ygyro, integrated_zgyro, temperature, quality, time_delta_distance_us, distance):
                '''
                Simulated optical flow from a flow sensor (e.g. PX4FLOW or optical
                mouse sensor)

                time_usec                 : Timestamp (microseconds, synced to UNIX time or since system boot) (uint64_t)
                sensor_id                 : Sensor ID (uint8_t)
                integration_time_us        : Integration time in microseconds. Divide integrated_x and integrated_y by the integration time to obtain average flow. The integration time also indicates the. (uint32_t)
                integrated_x              : Flow in radians around X axis (Sensor RH rotation about the X axis induces a positive flow. Sensor linear motion along the positive Y axis induces a negative flow.) (float)
                integrated_y              : Flow in radians around Y axis (Sensor RH rotation about the Y axis induces a positive flow. Sensor linear motion along the positive X axis induces a positive flow.) (float)
                integrated_xgyro          : RH rotation around X axis (rad) (float)
                integrated_ygyro          : RH rotation around Y axis (rad) (float)
                integrated_zgyro          : RH rotation around Z axis (rad) (float)
                temperature               : Temperature * 100 in centi-degrees Celsius (int16_t)
                quality                   : Optical flow quality / confidence. 0: no valid flow, 255: maximum quality (uint8_t)
                time_delta_distance_us        : Time in microseconds since the distance was sampled. (uint32_t)
                distance                  : Distance to the center of the flow field in meters. Positive value (including zero): distance known. Negative value: Unknown distance. (float)

                '''
                return self.send(self.hil_optical_flow_encode(time_usec, sensor_id, integration_time_us, integrated_x, integrated_y, integrated_xgyro, integrated_ygyro, integrated_zgyro, temperature, quality, time_delta_distance_us, distance))

        def hil_state_quaternion_encode(self, time_usec, attitude_quaternion, rollspeed, pitchspeed, yawspeed, lat, lon, alt, vx, vy, vz, ind_airspeed, true_airspeed, xacc, yacc, zacc):
                '''
                Sent from simulation to autopilot, avoids in contrast to HIL_STATE
                singularities. This packet is useful for high
                throughput applications such as hardware in the loop
                simulations.

                time_usec                 : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
                attitude_quaternion        : Vehicle attitude expressed as normalized quaternion in w, x, y, z order (with 1 0 0 0 being the null-rotation) (float)
                rollspeed                 : Body frame roll / phi angular speed (rad/s) (float)
                pitchspeed                : Body frame pitch / theta angular speed (rad/s) (float)
                yawspeed                  : Body frame yaw / psi angular speed (rad/s) (float)
                lat                       : Latitude, expressed as * 1E7 (int32_t)
                lon                       : Longitude, expressed as * 1E7 (int32_t)
                alt                       : Altitude in meters, expressed as * 1000 (millimeters) (int32_t)
                vx                        : Ground X Speed (Latitude), expressed as m/s * 100 (int16_t)
                vy                        : Ground Y Speed (Longitude), expressed as m/s * 100 (int16_t)
                vz                        : Ground Z Speed (Altitude), expressed as m/s * 100 (int16_t)
                ind_airspeed              : Indicated airspeed, expressed as m/s * 100 (uint16_t)
                true_airspeed             : True airspeed, expressed as m/s * 100 (uint16_t)
                xacc                      : X acceleration (mg) (int16_t)
                yacc                      : Y acceleration (mg) (int16_t)
                zacc                      : Z acceleration (mg) (int16_t)

                '''
                return MAVLink_hil_state_quaternion_message(time_usec, attitude_quaternion, rollspeed, pitchspeed, yawspeed, lat, lon, alt, vx, vy, vz, ind_airspeed, true_airspeed, xacc, yacc, zacc)

        def hil_state_quaternion_send(self, time_usec, attitude_quaternion, rollspeed, pitchspeed, yawspeed, lat, lon, alt, vx, vy, vz, ind_airspeed, true_airspeed, xacc, yacc, zacc):
                '''
                Sent from simulation to autopilot, avoids in contrast to HIL_STATE
                singularities. This packet is useful for high
                throughput applications such as hardware in the loop
                simulations.

                time_usec                 : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
                attitude_quaternion        : Vehicle attitude expressed as normalized quaternion in w, x, y, z order (with 1 0 0 0 being the null-rotation) (float)
                rollspeed                 : Body frame roll / phi angular speed (rad/s) (float)
                pitchspeed                : Body frame pitch / theta angular speed (rad/s) (float)
                yawspeed                  : Body frame yaw / psi angular speed (rad/s) (float)
                lat                       : Latitude, expressed as * 1E7 (int32_t)
                lon                       : Longitude, expressed as * 1E7 (int32_t)
                alt                       : Altitude in meters, expressed as * 1000 (millimeters) (int32_t)
                vx                        : Ground X Speed (Latitude), expressed as m/s * 100 (int16_t)
                vy                        : Ground Y Speed (Longitude), expressed as m/s * 100 (int16_t)
                vz                        : Ground Z Speed (Altitude), expressed as m/s * 100 (int16_t)
                ind_airspeed              : Indicated airspeed, expressed as m/s * 100 (uint16_t)
                true_airspeed             : True airspeed, expressed as m/s * 100 (uint16_t)
                xacc                      : X acceleration (mg) (int16_t)
                yacc                      : Y acceleration (mg) (int16_t)
                zacc                      : Z acceleration (mg) (int16_t)

                '''
                return self.send(self.hil_state_quaternion_encode(time_usec, attitude_quaternion, rollspeed, pitchspeed, yawspeed, lat, lon, alt, vx, vy, vz, ind_airspeed, true_airspeed, xacc, yacc, zacc))

        def scaled_imu2_encode(self, time_boot_ms, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag):
                '''
                The RAW IMU readings for secondary 9DOF sensor setup. This message
                should contain the scaled values to the described
                units

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                xacc                      : X acceleration (mg) (int16_t)
                yacc                      : Y acceleration (mg) (int16_t)
                zacc                      : Z acceleration (mg) (int16_t)
                xgyro                     : Angular speed around X axis (millirad /sec) (int16_t)
                ygyro                     : Angular speed around Y axis (millirad /sec) (int16_t)
                zgyro                     : Angular speed around Z axis (millirad /sec) (int16_t)
                xmag                      : X Magnetic field (milli tesla) (int16_t)
                ymag                      : Y Magnetic field (milli tesla) (int16_t)
                zmag                      : Z Magnetic field (milli tesla) (int16_t)

                '''
                return MAVLink_scaled_imu2_message(time_boot_ms, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag)

        def scaled_imu2_send(self, time_boot_ms, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag):
                '''
                The RAW IMU readings for secondary 9DOF sensor setup. This message
                should contain the scaled values to the described
                units

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                xacc                      : X acceleration (mg) (int16_t)
                yacc                      : Y acceleration (mg) (int16_t)
                zacc                      : Z acceleration (mg) (int16_t)
                xgyro                     : Angular speed around X axis (millirad /sec) (int16_t)
                ygyro                     : Angular speed around Y axis (millirad /sec) (int16_t)
                zgyro                     : Angular speed around Z axis (millirad /sec) (int16_t)
                xmag                      : X Magnetic field (milli tesla) (int16_t)
                ymag                      : Y Magnetic field (milli tesla) (int16_t)
                zmag                      : Z Magnetic field (milli tesla) (int16_t)

                '''
                return self.send(self.scaled_imu2_encode(time_boot_ms, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag))

        def log_request_list_encode(self, target_system, target_component, start, end):
                '''
                Request a list of available logs. On some systems calling this may
                stop on-board logging until LOG_REQUEST_END is called.

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                start                     : First log id (0 for first available) (uint16_t)
                end                       : Last log id (0xffff for last available) (uint16_t)

                '''
                return MAVLink_log_request_list_message(target_system, target_component, start, end)

        def log_request_list_send(self, target_system, target_component, start, end):
                '''
                Request a list of available logs. On some systems calling this may
                stop on-board logging until LOG_REQUEST_END is called.

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                start                     : First log id (0 for first available) (uint16_t)
                end                       : Last log id (0xffff for last available) (uint16_t)

                '''
                return self.send(self.log_request_list_encode(target_system, target_component, start, end))

        def log_entry_encode(self, id, num_logs, last_log_num, time_utc, size):
                '''
                Reply to LOG_REQUEST_LIST

                id                        : Log id (uint16_t)
                num_logs                  : Total number of logs (uint16_t)
                last_log_num              : High log number (uint16_t)
                time_utc                  : UTC timestamp of log in seconds since 1970, or 0 if not available (uint32_t)
                size                      : Size of the log (may be approximate) in bytes (uint32_t)

                '''
                return MAVLink_log_entry_message(id, num_logs, last_log_num, time_utc, size)

        def log_entry_send(self, id, num_logs, last_log_num, time_utc, size):
                '''
                Reply to LOG_REQUEST_LIST

                id                        : Log id (uint16_t)
                num_logs                  : Total number of logs (uint16_t)
                last_log_num              : High log number (uint16_t)
                time_utc                  : UTC timestamp of log in seconds since 1970, or 0 if not available (uint32_t)
                size                      : Size of the log (may be approximate) in bytes (uint32_t)

                '''
                return self.send(self.log_entry_encode(id, num_logs, last_log_num, time_utc, size))

        def log_request_data_encode(self, target_system, target_component, id, ofs, count):
                '''
                Request a chunk of a log

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                id                        : Log id (from LOG_ENTRY reply) (uint16_t)
                ofs                       : Offset into the log (uint32_t)
                count                     : Number of bytes (uint32_t)

                '''
                return MAVLink_log_request_data_message(target_system, target_component, id, ofs, count)

        def log_request_data_send(self, target_system, target_component, id, ofs, count):
                '''
                Request a chunk of a log

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                id                        : Log id (from LOG_ENTRY reply) (uint16_t)
                ofs                       : Offset into the log (uint32_t)
                count                     : Number of bytes (uint32_t)

                '''
                return self.send(self.log_request_data_encode(target_system, target_component, id, ofs, count))

        def log_data_encode(self, id, ofs, count, data):
                '''
                Reply to LOG_REQUEST_DATA

                id                        : Log id (from LOG_ENTRY reply) (uint16_t)
                ofs                       : Offset into the log (uint32_t)
                count                     : Number of bytes (zero for end of log) (uint8_t)
                data                      : log data (uint8_t)

                '''
                return MAVLink_log_data_message(id, ofs, count, data)

        def log_data_send(self, id, ofs, count, data):
                '''
                Reply to LOG_REQUEST_DATA

                id                        : Log id (from LOG_ENTRY reply) (uint16_t)
                ofs                       : Offset into the log (uint32_t)
                count                     : Number of bytes (zero for end of log) (uint8_t)
                data                      : log data (uint8_t)

                '''
                return self.send(self.log_data_encode(id, ofs, count, data))

        def log_erase_encode(self, target_system, target_component):
                '''
                Erase all logs

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)

                '''
                return MAVLink_log_erase_message(target_system, target_component)

        def log_erase_send(self, target_system, target_component):
                '''
                Erase all logs

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)

                '''
                return self.send(self.log_erase_encode(target_system, target_component))

        def log_request_end_encode(self, target_system, target_component):
                '''
                Stop log transfer and resume normal logging

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)

                '''
                return MAVLink_log_request_end_message(target_system, target_component)

        def log_request_end_send(self, target_system, target_component):
                '''
                Stop log transfer and resume normal logging

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)

                '''
                return self.send(self.log_request_end_encode(target_system, target_component))

        def gps_inject_data_encode(self, target_system, target_component, len, data):
                '''
                data for injecting into the onboard GPS (used for DGPS)

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                len                       : data length (uint8_t)
                data                      : raw data (110 is enough for 12 satellites of RTCMv2) (uint8_t)

                '''
                return MAVLink_gps_inject_data_message(target_system, target_component, len, data)

        def gps_inject_data_send(self, target_system, target_component, len, data):
                '''
                data for injecting into the onboard GPS (used for DGPS)

                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                len                       : data length (uint8_t)
                data                      : raw data (110 is enough for 12 satellites of RTCMv2) (uint8_t)

                '''
                return self.send(self.gps_inject_data_encode(target_system, target_component, len, data))

        def gps2_raw_encode(self, time_usec, fix_type, lat, lon, alt, eph, epv, vel, cog, satellites_visible, dgps_numch, dgps_age):
                '''
                Second GPS data. Coordinate frame is right-handed, Z-axis up (GPS
                frame).

                time_usec                 : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
                fix_type                  : 0-1: no fix, 2: 2D fix, 3: 3D fix, 4: DGPS fix, 5: RTK Fix. Some applications will not use the value of this field unless it is at least two, so always correctly fill in the fix. (uint8_t)
                lat                       : Latitude (WGS84), in degrees * 1E7 (int32_t)
                lon                       : Longitude (WGS84), in degrees * 1E7 (int32_t)
                alt                       : Altitude (AMSL, not WGS84), in meters * 1000 (positive for up) (int32_t)
                eph                       : GPS HDOP horizontal dilution of position in cm (m*100). If unknown, set to: UINT16_MAX (uint16_t)
                epv                       : GPS VDOP vertical dilution of position in cm (m*100). If unknown, set to: UINT16_MAX (uint16_t)
                vel                       : GPS ground speed (m/s * 100). If unknown, set to: UINT16_MAX (uint16_t)
                cog                       : Course over ground (NOT heading, but direction of movement) in degrees * 100, 0.0..359.99 degrees. If unknown, set to: UINT16_MAX (uint16_t)
                satellites_visible        : Number of satellites visible. If unknown, set to 255 (uint8_t)
                dgps_numch                : Number of DGPS satellites (uint8_t)
                dgps_age                  : Age of DGPS info (uint32_t)

                '''
                return MAVLink_gps2_raw_message(time_usec, fix_type, lat, lon, alt, eph, epv, vel, cog, satellites_visible, dgps_numch, dgps_age)

        def gps2_raw_send(self, time_usec, fix_type, lat, lon, alt, eph, epv, vel, cog, satellites_visible, dgps_numch, dgps_age):
                '''
                Second GPS data. Coordinate frame is right-handed, Z-axis up (GPS
                frame).

                time_usec                 : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
                fix_type                  : 0-1: no fix, 2: 2D fix, 3: 3D fix, 4: DGPS fix, 5: RTK Fix. Some applications will not use the value of this field unless it is at least two, so always correctly fill in the fix. (uint8_t)
                lat                       : Latitude (WGS84), in degrees * 1E7 (int32_t)
                lon                       : Longitude (WGS84), in degrees * 1E7 (int32_t)
                alt                       : Altitude (AMSL, not WGS84), in meters * 1000 (positive for up) (int32_t)
                eph                       : GPS HDOP horizontal dilution of position in cm (m*100). If unknown, set to: UINT16_MAX (uint16_t)
                epv                       : GPS VDOP vertical dilution of position in cm (m*100). If unknown, set to: UINT16_MAX (uint16_t)
                vel                       : GPS ground speed (m/s * 100). If unknown, set to: UINT16_MAX (uint16_t)
                cog                       : Course over ground (NOT heading, but direction of movement) in degrees * 100, 0.0..359.99 degrees. If unknown, set to: UINT16_MAX (uint16_t)
                satellites_visible        : Number of satellites visible. If unknown, set to 255 (uint8_t)
                dgps_numch                : Number of DGPS satellites (uint8_t)
                dgps_age                  : Age of DGPS info (uint32_t)

                '''
                return self.send(self.gps2_raw_encode(time_usec, fix_type, lat, lon, alt, eph, epv, vel, cog, satellites_visible, dgps_numch, dgps_age))

        def power_status_encode(self, Vcc, Vservo, flags):
                '''
                Power supply status

                Vcc                       : 5V rail voltage in millivolts (uint16_t)
                Vservo                    : servo rail voltage in millivolts (uint16_t)
                flags                     : power supply status flags (see MAV_POWER_STATUS enum) (uint16_t)

                '''
                return MAVLink_power_status_message(Vcc, Vservo, flags)

        def power_status_send(self, Vcc, Vservo, flags):
                '''
                Power supply status

                Vcc                       : 5V rail voltage in millivolts (uint16_t)
                Vservo                    : servo rail voltage in millivolts (uint16_t)
                flags                     : power supply status flags (see MAV_POWER_STATUS enum) (uint16_t)

                '''
                return self.send(self.power_status_encode(Vcc, Vservo, flags))

        def serial_control_encode(self, device, flags, timeout, baudrate, count, data):
                '''
                Control a serial port. This can be used for raw access to an onboard
                serial peripheral such as a GPS or telemetry radio. It
                is designed to make it possible to update the devices
                firmware via MAVLink messages or change the devices
                settings. A message with zero bytes can be used to
                change just the baudrate.

                device                    : See SERIAL_CONTROL_DEV enum (uint8_t)
                flags                     : See SERIAL_CONTROL_FLAG enum (uint8_t)
                timeout                   : Timeout for reply data in milliseconds (uint16_t)
                baudrate                  : Baudrate of transfer. Zero means no change. (uint32_t)
                count                     : how many bytes in this transfer (uint8_t)
                data                      : serial data (uint8_t)

                '''
                return MAVLink_serial_control_message(device, flags, timeout, baudrate, count, data)

        def serial_control_send(self, device, flags, timeout, baudrate, count, data):
                '''
                Control a serial port. This can be used for raw access to an onboard
                serial peripheral such as a GPS or telemetry radio. It
                is designed to make it possible to update the devices
                firmware via MAVLink messages or change the devices
                settings. A message with zero bytes can be used to
                change just the baudrate.

                device                    : See SERIAL_CONTROL_DEV enum (uint8_t)
                flags                     : See SERIAL_CONTROL_FLAG enum (uint8_t)
                timeout                   : Timeout for reply data in milliseconds (uint16_t)
                baudrate                  : Baudrate of transfer. Zero means no change. (uint32_t)
                count                     : how many bytes in this transfer (uint8_t)
                data                      : serial data (uint8_t)

                '''
                return self.send(self.serial_control_encode(device, flags, timeout, baudrate, count, data))

        def gps_rtk_encode(self, time_last_baseline_ms, rtk_receiver_id, wn, tow, rtk_health, rtk_rate, nsats, baseline_coords_type, baseline_a_mm, baseline_b_mm, baseline_c_mm, accuracy, iar_num_hypotheses):
                '''
                RTK GPS data. Gives information on the relative baseline calculation
                the GPS is reporting

                time_last_baseline_ms        : Time since boot of last baseline message received in ms. (uint32_t)
                rtk_receiver_id           : Identification of connected RTK receiver. (uint8_t)
                wn                        : GPS Week Number of last baseline (uint16_t)
                tow                       : GPS Time of Week of last baseline (uint32_t)
                rtk_health                : GPS-specific health report for RTK data. (uint8_t)
                rtk_rate                  : Rate of baseline messages being received by GPS, in HZ (uint8_t)
                nsats                     : Current number of sats used for RTK calculation. (uint8_t)
                baseline_coords_type        : Coordinate system of baseline. 0 == ECEF, 1 == NED (uint8_t)
                baseline_a_mm             : Current baseline in ECEF x or NED north component in mm. (int32_t)
                baseline_b_mm             : Current baseline in ECEF y or NED east component in mm. (int32_t)
                baseline_c_mm             : Current baseline in ECEF z or NED down component in mm. (int32_t)
                accuracy                  : Current estimate of baseline accuracy. (uint32_t)
                iar_num_hypotheses        : Current number of integer ambiguity hypotheses. (int32_t)

                '''
                return MAVLink_gps_rtk_message(time_last_baseline_ms, rtk_receiver_id, wn, tow, rtk_health, rtk_rate, nsats, baseline_coords_type, baseline_a_mm, baseline_b_mm, baseline_c_mm, accuracy, iar_num_hypotheses)

        def gps_rtk_send(self, time_last_baseline_ms, rtk_receiver_id, wn, tow, rtk_health, rtk_rate, nsats, baseline_coords_type, baseline_a_mm, baseline_b_mm, baseline_c_mm, accuracy, iar_num_hypotheses):
                '''
                RTK GPS data. Gives information on the relative baseline calculation
                the GPS is reporting

                time_last_baseline_ms        : Time since boot of last baseline message received in ms. (uint32_t)
                rtk_receiver_id           : Identification of connected RTK receiver. (uint8_t)
                wn                        : GPS Week Number of last baseline (uint16_t)
                tow                       : GPS Time of Week of last baseline (uint32_t)
                rtk_health                : GPS-specific health report for RTK data. (uint8_t)
                rtk_rate                  : Rate of baseline messages being received by GPS, in HZ (uint8_t)
                nsats                     : Current number of sats used for RTK calculation. (uint8_t)
                baseline_coords_type        : Coordinate system of baseline. 0 == ECEF, 1 == NED (uint8_t)
                baseline_a_mm             : Current baseline in ECEF x or NED north component in mm. (int32_t)
                baseline_b_mm             : Current baseline in ECEF y or NED east component in mm. (int32_t)
                baseline_c_mm             : Current baseline in ECEF z or NED down component in mm. (int32_t)
                accuracy                  : Current estimate of baseline accuracy. (uint32_t)
                iar_num_hypotheses        : Current number of integer ambiguity hypotheses. (int32_t)

                '''
                return self.send(self.gps_rtk_encode(time_last_baseline_ms, rtk_receiver_id, wn, tow, rtk_health, rtk_rate, nsats, baseline_coords_type, baseline_a_mm, baseline_b_mm, baseline_c_mm, accuracy, iar_num_hypotheses))

        def gps2_rtk_encode(self, time_last_baseline_ms, rtk_receiver_id, wn, tow, rtk_health, rtk_rate, nsats, baseline_coords_type, baseline_a_mm, baseline_b_mm, baseline_c_mm, accuracy, iar_num_hypotheses):
                '''
                RTK GPS data. Gives information on the relative baseline calculation
                the GPS is reporting

                time_last_baseline_ms        : Time since boot of last baseline message received in ms. (uint32_t)
                rtk_receiver_id           : Identification of connected RTK receiver. (uint8_t)
                wn                        : GPS Week Number of last baseline (uint16_t)
                tow                       : GPS Time of Week of last baseline (uint32_t)
                rtk_health                : GPS-specific health report for RTK data. (uint8_t)
                rtk_rate                  : Rate of baseline messages being received by GPS, in HZ (uint8_t)
                nsats                     : Current number of sats used for RTK calculation. (uint8_t)
                baseline_coords_type        : Coordinate system of baseline. 0 == ECEF, 1 == NED (uint8_t)
                baseline_a_mm             : Current baseline in ECEF x or NED north component in mm. (int32_t)
                baseline_b_mm             : Current baseline in ECEF y or NED east component in mm. (int32_t)
                baseline_c_mm             : Current baseline in ECEF z or NED down component in mm. (int32_t)
                accuracy                  : Current estimate of baseline accuracy. (uint32_t)
                iar_num_hypotheses        : Current number of integer ambiguity hypotheses. (int32_t)

                '''
                return MAVLink_gps2_rtk_message(time_last_baseline_ms, rtk_receiver_id, wn, tow, rtk_health, rtk_rate, nsats, baseline_coords_type, baseline_a_mm, baseline_b_mm, baseline_c_mm, accuracy, iar_num_hypotheses)

        def gps2_rtk_send(self, time_last_baseline_ms, rtk_receiver_id, wn, tow, rtk_health, rtk_rate, nsats, baseline_coords_type, baseline_a_mm, baseline_b_mm, baseline_c_mm, accuracy, iar_num_hypotheses):
                '''
                RTK GPS data. Gives information on the relative baseline calculation
                the GPS is reporting

                time_last_baseline_ms        : Time since boot of last baseline message received in ms. (uint32_t)
                rtk_receiver_id           : Identification of connected RTK receiver. (uint8_t)
                wn                        : GPS Week Number of last baseline (uint16_t)
                tow                       : GPS Time of Week of last baseline (uint32_t)
                rtk_health                : GPS-specific health report for RTK data. (uint8_t)
                rtk_rate                  : Rate of baseline messages being received by GPS, in HZ (uint8_t)
                nsats                     : Current number of sats used for RTK calculation. (uint8_t)
                baseline_coords_type        : Coordinate system of baseline. 0 == ECEF, 1 == NED (uint8_t)
                baseline_a_mm             : Current baseline in ECEF x or NED north component in mm. (int32_t)
                baseline_b_mm             : Current baseline in ECEF y or NED east component in mm. (int32_t)
                baseline_c_mm             : Current baseline in ECEF z or NED down component in mm. (int32_t)
                accuracy                  : Current estimate of baseline accuracy. (uint32_t)
                iar_num_hypotheses        : Current number of integer ambiguity hypotheses. (int32_t)

                '''
                return self.send(self.gps2_rtk_encode(time_last_baseline_ms, rtk_receiver_id, wn, tow, rtk_health, rtk_rate, nsats, baseline_coords_type, baseline_a_mm, baseline_b_mm, baseline_c_mm, accuracy, iar_num_hypotheses))

        def scaled_imu3_encode(self, time_boot_ms, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag):
                '''
                The RAW IMU readings for 3rd 9DOF sensor setup. This message should
                contain the scaled values to the described units

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                xacc                      : X acceleration (mg) (int16_t)
                yacc                      : Y acceleration (mg) (int16_t)
                zacc                      : Z acceleration (mg) (int16_t)
                xgyro                     : Angular speed around X axis (millirad /sec) (int16_t)
                ygyro                     : Angular speed around Y axis (millirad /sec) (int16_t)
                zgyro                     : Angular speed around Z axis (millirad /sec) (int16_t)
                xmag                      : X Magnetic field (milli tesla) (int16_t)
                ymag                      : Y Magnetic field (milli tesla) (int16_t)
                zmag                      : Z Magnetic field (milli tesla) (int16_t)

                '''
                return MAVLink_scaled_imu3_message(time_boot_ms, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag)

        def scaled_imu3_send(self, time_boot_ms, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag):
                '''
                The RAW IMU readings for 3rd 9DOF sensor setup. This message should
                contain the scaled values to the described units

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                xacc                      : X acceleration (mg) (int16_t)
                yacc                      : Y acceleration (mg) (int16_t)
                zacc                      : Z acceleration (mg) (int16_t)
                xgyro                     : Angular speed around X axis (millirad /sec) (int16_t)
                ygyro                     : Angular speed around Y axis (millirad /sec) (int16_t)
                zgyro                     : Angular speed around Z axis (millirad /sec) (int16_t)
                xmag                      : X Magnetic field (milli tesla) (int16_t)
                ymag                      : Y Magnetic field (milli tesla) (int16_t)
                zmag                      : Z Magnetic field (milli tesla) (int16_t)

                '''
                return self.send(self.scaled_imu3_encode(time_boot_ms, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag))

        def data_transmission_handshake_encode(self, type, size, width, height, packets, payload, jpg_quality):
                '''
                

                type                      : type of requested/acknowledged data (as defined in ENUM DATA_TYPES in mavlink/include/mavlink_types.h) (uint8_t)
                size                      : total data size in bytes (set on ACK only) (uint32_t)
                width                     : Width of a matrix or image (uint16_t)
                height                    : Height of a matrix or image (uint16_t)
                packets                   : number of packets beeing sent (set on ACK only) (uint16_t)
                payload                   : payload size per packet (normally 253 byte, see DATA field size in message ENCAPSULATED_DATA) (set on ACK only) (uint8_t)
                jpg_quality               : JPEG quality out of [1,100] (uint8_t)

                '''
                return MAVLink_data_transmission_handshake_message(type, size, width, height, packets, payload, jpg_quality)

        def data_transmission_handshake_send(self, type, size, width, height, packets, payload, jpg_quality):
                '''
                

                type                      : type of requested/acknowledged data (as defined in ENUM DATA_TYPES in mavlink/include/mavlink_types.h) (uint8_t)
                size                      : total data size in bytes (set on ACK only) (uint32_t)
                width                     : Width of a matrix or image (uint16_t)
                height                    : Height of a matrix or image (uint16_t)
                packets                   : number of packets beeing sent (set on ACK only) (uint16_t)
                payload                   : payload size per packet (normally 253 byte, see DATA field size in message ENCAPSULATED_DATA) (set on ACK only) (uint8_t)
                jpg_quality               : JPEG quality out of [1,100] (uint8_t)

                '''
                return self.send(self.data_transmission_handshake_encode(type, size, width, height, packets, payload, jpg_quality))

        def encapsulated_data_encode(self, seqnr, data):
                '''
                

                seqnr                     : sequence number (starting with 0 on every transmission) (uint16_t)
                data                      : image data bytes (uint8_t)

                '''
                return MAVLink_encapsulated_data_message(seqnr, data)

        def encapsulated_data_send(self, seqnr, data):
                '''
                

                seqnr                     : sequence number (starting with 0 on every transmission) (uint16_t)
                data                      : image data bytes (uint8_t)

                '''
                return self.send(self.encapsulated_data_encode(seqnr, data))

        def distance_sensor_encode(self, time_boot_ms, min_distance, max_distance, current_distance, type, id, orientation, covariance):
                '''
                

                time_boot_ms              : Time since system boot (uint32_t)
                min_distance              : Minimum distance the sensor can measure in centimeters (uint16_t)
                max_distance              : Maximum distance the sensor can measure in centimeters (uint16_t)
                current_distance          : Current distance reading (uint16_t)
                type                      : Type from MAV_DISTANCE_SENSOR enum. (uint8_t)
                id                        : Onboard ID of the sensor (uint8_t)
                orientation               : Direction the sensor faces from MAV_SENSOR_ORIENTATION enum. (uint8_t)
                covariance                : Measurement covariance in centimeters, 0 for unknown / invalid readings (uint8_t)

                '''
                return MAVLink_distance_sensor_message(time_boot_ms, min_distance, max_distance, current_distance, type, id, orientation, covariance)

        def distance_sensor_send(self, time_boot_ms, min_distance, max_distance, current_distance, type, id, orientation, covariance):
                '''
                

                time_boot_ms              : Time since system boot (uint32_t)
                min_distance              : Minimum distance the sensor can measure in centimeters (uint16_t)
                max_distance              : Maximum distance the sensor can measure in centimeters (uint16_t)
                current_distance          : Current distance reading (uint16_t)
                type                      : Type from MAV_DISTANCE_SENSOR enum. (uint8_t)
                id                        : Onboard ID of the sensor (uint8_t)
                orientation               : Direction the sensor faces from MAV_SENSOR_ORIENTATION enum. (uint8_t)
                covariance                : Measurement covariance in centimeters, 0 for unknown / invalid readings (uint8_t)

                '''
                return self.send(self.distance_sensor_encode(time_boot_ms, min_distance, max_distance, current_distance, type, id, orientation, covariance))

        def terrain_request_encode(self, lat, lon, grid_spacing, mask):
                '''
                Request for terrain data and terrain status

                lat                       : Latitude of SW corner of first grid (degrees *10^7) (int32_t)
                lon                       : Longitude of SW corner of first grid (in degrees *10^7) (int32_t)
                grid_spacing              : Grid spacing in meters (uint16_t)
                mask                      : Bitmask of requested 4x4 grids (row major 8x7 array of grids, 56 bits) (uint64_t)

                '''
                return MAVLink_terrain_request_message(lat, lon, grid_spacing, mask)

        def terrain_request_send(self, lat, lon, grid_spacing, mask):
                '''
                Request for terrain data and terrain status

                lat                       : Latitude of SW corner of first grid (degrees *10^7) (int32_t)
                lon                       : Longitude of SW corner of first grid (in degrees *10^7) (int32_t)
                grid_spacing              : Grid spacing in meters (uint16_t)
                mask                      : Bitmask of requested 4x4 grids (row major 8x7 array of grids, 56 bits) (uint64_t)

                '''
                return self.send(self.terrain_request_encode(lat, lon, grid_spacing, mask))

        def terrain_data_encode(self, lat, lon, grid_spacing, gridbit, data):
                '''
                Terrain data sent from GCS. The lat/lon and grid_spacing must be the
                same as a lat/lon from a TERRAIN_REQUEST

                lat                       : Latitude of SW corner of first grid (degrees *10^7) (int32_t)
                lon                       : Longitude of SW corner of first grid (in degrees *10^7) (int32_t)
                grid_spacing              : Grid spacing in meters (uint16_t)
                gridbit                   : bit within the terrain request mask (uint8_t)
                data                      : Terrain data in meters AMSL (int16_t)

                '''
                return MAVLink_terrain_data_message(lat, lon, grid_spacing, gridbit, data)

        def terrain_data_send(self, lat, lon, grid_spacing, gridbit, data):
                '''
                Terrain data sent from GCS. The lat/lon and grid_spacing must be the
                same as a lat/lon from a TERRAIN_REQUEST

                lat                       : Latitude of SW corner of first grid (degrees *10^7) (int32_t)
                lon                       : Longitude of SW corner of first grid (in degrees *10^7) (int32_t)
                grid_spacing              : Grid spacing in meters (uint16_t)
                gridbit                   : bit within the terrain request mask (uint8_t)
                data                      : Terrain data in meters AMSL (int16_t)

                '''
                return self.send(self.terrain_data_encode(lat, lon, grid_spacing, gridbit, data))

        def terrain_check_encode(self, lat, lon):
                '''
                Request that the vehicle report terrain height at the given location.
                Used by GCS to check if vehicle has all terrain data
                needed for a mission.

                lat                       : Latitude (degrees *10^7) (int32_t)
                lon                       : Longitude (degrees *10^7) (int32_t)

                '''
                return MAVLink_terrain_check_message(lat, lon)

        def terrain_check_send(self, lat, lon):
                '''
                Request that the vehicle report terrain height at the given location.
                Used by GCS to check if vehicle has all terrain data
                needed for a mission.

                lat                       : Latitude (degrees *10^7) (int32_t)
                lon                       : Longitude (degrees *10^7) (int32_t)

                '''
                return self.send(self.terrain_check_encode(lat, lon))

        def terrain_report_encode(self, lat, lon, spacing, terrain_height, current_height, pending, loaded):
                '''
                Response from a TERRAIN_CHECK request

                lat                       : Latitude (degrees *10^7) (int32_t)
                lon                       : Longitude (degrees *10^7) (int32_t)
                spacing                   : grid spacing (zero if terrain at this location unavailable) (uint16_t)
                terrain_height            : Terrain height in meters AMSL (float)
                current_height            : Current vehicle height above lat/lon terrain height (meters) (float)
                pending                   : Number of 4x4 terrain blocks waiting to be received or read from disk (uint16_t)
                loaded                    : Number of 4x4 terrain blocks in memory (uint16_t)

                '''
                return MAVLink_terrain_report_message(lat, lon, spacing, terrain_height, current_height, pending, loaded)

        def terrain_report_send(self, lat, lon, spacing, terrain_height, current_height, pending, loaded):
                '''
                Response from a TERRAIN_CHECK request

                lat                       : Latitude (degrees *10^7) (int32_t)
                lon                       : Longitude (degrees *10^7) (int32_t)
                spacing                   : grid spacing (zero if terrain at this location unavailable) (uint16_t)
                terrain_height            : Terrain height in meters AMSL (float)
                current_height            : Current vehicle height above lat/lon terrain height (meters) (float)
                pending                   : Number of 4x4 terrain blocks waiting to be received or read from disk (uint16_t)
                loaded                    : Number of 4x4 terrain blocks in memory (uint16_t)

                '''
                return self.send(self.terrain_report_encode(lat, lon, spacing, terrain_height, current_height, pending, loaded))

        def scaled_pressure2_encode(self, time_boot_ms, press_abs, press_diff, temperature):
                '''
                Barometer readings for 2nd barometer

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                press_abs                 : Absolute pressure (hectopascal) (float)
                press_diff                : Differential pressure 1 (hectopascal) (float)
                temperature               : Temperature measurement (0.01 degrees celsius) (int16_t)

                '''
                return MAVLink_scaled_pressure2_message(time_boot_ms, press_abs, press_diff, temperature)

        def scaled_pressure2_send(self, time_boot_ms, press_abs, press_diff, temperature):
                '''
                Barometer readings for 2nd barometer

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                press_abs                 : Absolute pressure (hectopascal) (float)
                press_diff                : Differential pressure 1 (hectopascal) (float)
                temperature               : Temperature measurement (0.01 degrees celsius) (int16_t)

                '''
                return self.send(self.scaled_pressure2_encode(time_boot_ms, press_abs, press_diff, temperature))

        def att_pos_mocap_encode(self, time_usec, q, x, y, z):
                '''
                Motion capture attitude and position

                time_usec                 : Timestamp (micros since boot or Unix epoch) (uint64_t)
                q                         : Attitude quaternion (w, x, y, z order, zero-rotation is 1, 0, 0, 0) (float)
                x                         : X position in meters (NED) (float)
                y                         : Y position in meters (NED) (float)
                z                         : Z position in meters (NED) (float)

                '''
                return MAVLink_att_pos_mocap_message(time_usec, q, x, y, z)

        def att_pos_mocap_send(self, time_usec, q, x, y, z):
                '''
                Motion capture attitude and position

                time_usec                 : Timestamp (micros since boot or Unix epoch) (uint64_t)
                q                         : Attitude quaternion (w, x, y, z order, zero-rotation is 1, 0, 0, 0) (float)
                x                         : X position in meters (NED) (float)
                y                         : Y position in meters (NED) (float)
                z                         : Z position in meters (NED) (float)

                '''
                return self.send(self.att_pos_mocap_encode(time_usec, q, x, y, z))

        def set_actuator_control_target_encode(self, time_usec, group_mlx, target_system, target_component, controls):
                '''
                Set the vehicle attitude and body angular rates.

                time_usec                 : Timestamp (micros since boot or Unix epoch) (uint64_t)
                group_mlx                 : Actuator group. The "_mlx" indicates this is a multi-instance message and a MAVLink parser should use this field to difference between instances. (uint8_t)
                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                controls                  : Actuator controls. Normed to -1..+1 where 0 is neutral position. Throttle for single rotation direction motors is 0..1, negative range for reverse direction. Standard mapping for attitude controls (group 0): (index 0-7): roll, pitch, yaw, throttle, flaps, spoilers, airbrakes, landing gear. Load a pass-through mixer to repurpose them as generic outputs. (float)

                '''
                return MAVLink_set_actuator_control_target_message(time_usec, group_mlx, target_system, target_component, controls)

        def set_actuator_control_target_send(self, time_usec, group_mlx, target_system, target_component, controls):
                '''
                Set the vehicle attitude and body angular rates.

                time_usec                 : Timestamp (micros since boot or Unix epoch) (uint64_t)
                group_mlx                 : Actuator group. The "_mlx" indicates this is a multi-instance message and a MAVLink parser should use this field to difference between instances. (uint8_t)
                target_system             : System ID (uint8_t)
                target_component          : Component ID (uint8_t)
                controls                  : Actuator controls. Normed to -1..+1 where 0 is neutral position. Throttle for single rotation direction motors is 0..1, negative range for reverse direction. Standard mapping for attitude controls (group 0): (index 0-7): roll, pitch, yaw, throttle, flaps, spoilers, airbrakes, landing gear. Load a pass-through mixer to repurpose them as generic outputs. (float)

                '''
                return self.send(self.set_actuator_control_target_encode(time_usec, group_mlx, target_system, target_component, controls))

        def actuator_control_target_encode(self, time_usec, group_mlx, controls):
                '''
                Set the vehicle attitude and body angular rates.

                time_usec                 : Timestamp (micros since boot or Unix epoch) (uint64_t)
                group_mlx                 : Actuator group. The "_mlx" indicates this is a multi-instance message and a MAVLink parser should use this field to difference between instances. (uint8_t)
                controls                  : Actuator controls. Normed to -1..+1 where 0 is neutral position. Throttle for single rotation direction motors is 0..1, negative range for reverse direction. Standard mapping for attitude controls (group 0): (index 0-7): roll, pitch, yaw, throttle, flaps, spoilers, airbrakes, landing gear. Load a pass-through mixer to repurpose them as generic outputs. (float)

                '''
                return MAVLink_actuator_control_target_message(time_usec, group_mlx, controls)

        def actuator_control_target_send(self, time_usec, group_mlx, controls):
                '''
                Set the vehicle attitude and body angular rates.

                time_usec                 : Timestamp (micros since boot or Unix epoch) (uint64_t)
                group_mlx                 : Actuator group. The "_mlx" indicates this is a multi-instance message and a MAVLink parser should use this field to difference between instances. (uint8_t)
                controls                  : Actuator controls. Normed to -1..+1 where 0 is neutral position. Throttle for single rotation direction motors is 0..1, negative range for reverse direction. Standard mapping for attitude controls (group 0): (index 0-7): roll, pitch, yaw, throttle, flaps, spoilers, airbrakes, landing gear. Load a pass-through mixer to repurpose them as generic outputs. (float)

                '''
                return self.send(self.actuator_control_target_encode(time_usec, group_mlx, controls))

        def battery_status_encode(self, id, battery_function, type, temperature, voltages, current_battery, current_consumed, energy_consumed, battery_remaining):
                '''
                Battery information

                id                        : Battery ID (uint8_t)
                battery_function          : Function of the battery (uint8_t)
                type                      : Type (chemistry) of the battery (uint8_t)
                temperature               : Temperature of the battery in centi-degrees celsius. INT16_MAX for unknown temperature. (int16_t)
                voltages                  : Battery voltage of cells, in millivolts (1 = 1 millivolt) (uint16_t)
                current_battery           : Battery current, in 10*milliamperes (1 = 10 milliampere), -1: autopilot does not measure the current (int16_t)
                current_consumed          : Consumed charge, in milliampere hours (1 = 1 mAh), -1: autopilot does not provide mAh consumption estimate (int32_t)
                energy_consumed           : Consumed energy, in 100*Joules (intergrated U*I*dt)  (1 = 100 Joule), -1: autopilot does not provide energy consumption estimate (int32_t)
                battery_remaining         : Remaining battery energy: (0%: 0, 100%: 100), -1: autopilot does not estimate the remaining battery (int8_t)

                '''
                return MAVLink_battery_status_message(id, battery_function, type, temperature, voltages, current_battery, current_consumed, energy_consumed, battery_remaining)

        def battery_status_send(self, id, battery_function, type, temperature, voltages, current_battery, current_consumed, energy_consumed, battery_remaining):
                '''
                Battery information

                id                        : Battery ID (uint8_t)
                battery_function          : Function of the battery (uint8_t)
                type                      : Type (chemistry) of the battery (uint8_t)
                temperature               : Temperature of the battery in centi-degrees celsius. INT16_MAX for unknown temperature. (int16_t)
                voltages                  : Battery voltage of cells, in millivolts (1 = 1 millivolt) (uint16_t)
                current_battery           : Battery current, in 10*milliamperes (1 = 10 milliampere), -1: autopilot does not measure the current (int16_t)
                current_consumed          : Consumed charge, in milliampere hours (1 = 1 mAh), -1: autopilot does not provide mAh consumption estimate (int32_t)
                energy_consumed           : Consumed energy, in 100*Joules (intergrated U*I*dt)  (1 = 100 Joule), -1: autopilot does not provide energy consumption estimate (int32_t)
                battery_remaining         : Remaining battery energy: (0%: 0, 100%: 100), -1: autopilot does not estimate the remaining battery (int8_t)

                '''
                return self.send(self.battery_status_encode(id, battery_function, type, temperature, voltages, current_battery, current_consumed, energy_consumed, battery_remaining))

        def autopilot_version_encode(self, capabilities, flight_sw_version, middleware_sw_version, os_sw_version, board_version, flight_custom_version, middleware_custom_version, os_custom_version, vendor_id, product_id, uid):
                '''
                Version and capability of autopilot software

                capabilities              : bitmask of capabilities (see MAV_PROTOCOL_CAPABILITY enum) (uint64_t)
                flight_sw_version         : Firmware version number (uint32_t)
                middleware_sw_version        : Middleware version number (uint32_t)
                os_sw_version             : Operating system version number (uint32_t)
                board_version             : HW / board version (last 8 bytes should be silicon ID, if any) (uint32_t)
                flight_custom_version        : Custom version field, commonly the first 8 bytes of the git hash. This is not an unique identifier, but should allow to identify the commit using the main version number even for very large code bases. (uint8_t)
                middleware_custom_version        : Custom version field, commonly the first 8 bytes of the git hash. This is not an unique identifier, but should allow to identify the commit using the main version number even for very large code bases. (uint8_t)
                os_custom_version         : Custom version field, commonly the first 8 bytes of the git hash. This is not an unique identifier, but should allow to identify the commit using the main version number even for very large code bases. (uint8_t)
                vendor_id                 : ID of the board vendor (uint16_t)
                product_id                : ID of the product (uint16_t)
                uid                       : UID if provided by hardware (uint64_t)

                '''
                return MAVLink_autopilot_version_message(capabilities, flight_sw_version, middleware_sw_version, os_sw_version, board_version, flight_custom_version, middleware_custom_version, os_custom_version, vendor_id, product_id, uid)

        def autopilot_version_send(self, capabilities, flight_sw_version, middleware_sw_version, os_sw_version, board_version, flight_custom_version, middleware_custom_version, os_custom_version, vendor_id, product_id, uid):
                '''
                Version and capability of autopilot software

                capabilities              : bitmask of capabilities (see MAV_PROTOCOL_CAPABILITY enum) (uint64_t)
                flight_sw_version         : Firmware version number (uint32_t)
                middleware_sw_version        : Middleware version number (uint32_t)
                os_sw_version             : Operating system version number (uint32_t)
                board_version             : HW / board version (last 8 bytes should be silicon ID, if any) (uint32_t)
                flight_custom_version        : Custom version field, commonly the first 8 bytes of the git hash. This is not an unique identifier, but should allow to identify the commit using the main version number even for very large code bases. (uint8_t)
                middleware_custom_version        : Custom version field, commonly the first 8 bytes of the git hash. This is not an unique identifier, but should allow to identify the commit using the main version number even for very large code bases. (uint8_t)
                os_custom_version         : Custom version field, commonly the first 8 bytes of the git hash. This is not an unique identifier, but should allow to identify the commit using the main version number even for very large code bases. (uint8_t)
                vendor_id                 : ID of the board vendor (uint16_t)
                product_id                : ID of the product (uint16_t)
                uid                       : UID if provided by hardware (uint64_t)

                '''
                return self.send(self.autopilot_version_encode(capabilities, flight_sw_version, middleware_sw_version, os_sw_version, board_version, flight_custom_version, middleware_custom_version, os_custom_version, vendor_id, product_id, uid))

        def landing_target_encode(self, target_num, frame, angle_x, angle_y, distance):
                '''
                The location of a landing area captured from a downward facing camera

                target_num                : The ID of the target if multiple targets are present (uint8_t)
                frame                     : MAV_FRAME enum specifying the whether the following feilds are earth-frame, body-frame, etc. (uint8_t)
                angle_x                   : X-axis angular offset (in radians) of the target from the center of the image (float)
                angle_y                   : Y-axis angular offset (in radians) of the target from the center of the image (float)
                distance                  : Distance to the target from the vehicle in meters (float)

                '''
                return MAVLink_landing_target_message(target_num, frame, angle_x, angle_y, distance)

        def landing_target_send(self, target_num, frame, angle_x, angle_y, distance):
                '''
                The location of a landing area captured from a downward facing camera

                target_num                : The ID of the target if multiple targets are present (uint8_t)
                frame                     : MAV_FRAME enum specifying the whether the following feilds are earth-frame, body-frame, etc. (uint8_t)
                angle_x                   : X-axis angular offset (in radians) of the target from the center of the image (float)
                angle_y                   : Y-axis angular offset (in radians) of the target from the center of the image (float)
                distance                  : Distance to the target from the vehicle in meters (float)

                '''
                return self.send(self.landing_target_encode(target_num, frame, angle_x, angle_y, distance))

        def vibration_encode(self, time_usec, vibration_x, vibration_y, vibration_z, clipping_0, clipping_1, clipping_2):
                '''
                Vibration levels and accelerometer clipping

                time_usec                 : Timestamp (micros since boot or Unix epoch) (uint64_t)
                vibration_x               : Vibration levels on X-axis (float)
                vibration_y               : Vibration levels on Y-axis (float)
                vibration_z               : Vibration levels on Z-axis (float)
                clipping_0                : first accelerometer clipping count (uint32_t)
                clipping_1                : second accelerometer clipping count (uint32_t)
                clipping_2                : third accelerometer clipping count (uint32_t)

                '''
                return MAVLink_vibration_message(time_usec, vibration_x, vibration_y, vibration_z, clipping_0, clipping_1, clipping_2)

        def vibration_send(self, time_usec, vibration_x, vibration_y, vibration_z, clipping_0, clipping_1, clipping_2):
                '''
                Vibration levels and accelerometer clipping

                time_usec                 : Timestamp (micros since boot or Unix epoch) (uint64_t)
                vibration_x               : Vibration levels on X-axis (float)
                vibration_y               : Vibration levels on Y-axis (float)
                vibration_z               : Vibration levels on Z-axis (float)
                clipping_0                : first accelerometer clipping count (uint32_t)
                clipping_1                : second accelerometer clipping count (uint32_t)
                clipping_2                : third accelerometer clipping count (uint32_t)

                '''
                return self.send(self.vibration_encode(time_usec, vibration_x, vibration_y, vibration_z, clipping_0, clipping_1, clipping_2))

        def v2_extension_encode(self, target_network, target_system, target_component, message_type, payload):
                '''
                Message implementing parts of the V2 payload specs in V1 frames for
                transitional support.

                target_network            : Network ID (0 for broadcast) (uint8_t)
                target_system             : System ID (0 for broadcast) (uint8_t)
                target_component          : Component ID (0 for broadcast) (uint8_t)
                message_type              : A code that identifies the software component that understands this message (analogous to usb device classes or mime type strings).  If this code is less than 32768, it is considered a 'registered' protocol extension and the corresponding entry should be added to https://github.com/mavlink/mavlink/extension-message-ids.xml.  Software creators can register blocks of message IDs as needed (useful for GCS specific metadata, etc...). Message_types greater than 32767 are considered local experiments and should not be checked in to any widely distributed codebase. (uint16_t)
                payload                   : Variable length payload. The length is defined by the remaining message length when subtracting the header and other fields.  The entire content of this block is opaque unless you understand any the encoding message_type.  The particular encoding used can be extension specific and might not always be documented as part of the mavlink specification. (uint8_t)

                '''
                return MAVLink_v2_extension_message(target_network, target_system, target_component, message_type, payload)

        def v2_extension_send(self, target_network, target_system, target_component, message_type, payload):
                '''
                Message implementing parts of the V2 payload specs in V1 frames for
                transitional support.

                target_network            : Network ID (0 for broadcast) (uint8_t)
                target_system             : System ID (0 for broadcast) (uint8_t)
                target_component          : Component ID (0 for broadcast) (uint8_t)
                message_type              : A code that identifies the software component that understands this message (analogous to usb device classes or mime type strings).  If this code is less than 32768, it is considered a 'registered' protocol extension and the corresponding entry should be added to https://github.com/mavlink/mavlink/extension-message-ids.xml.  Software creators can register blocks of message IDs as needed (useful for GCS specific metadata, etc...). Message_types greater than 32767 are considered local experiments and should not be checked in to any widely distributed codebase. (uint16_t)
                payload                   : Variable length payload. The length is defined by the remaining message length when subtracting the header and other fields.  The entire content of this block is opaque unless you understand any the encoding message_type.  The particular encoding used can be extension specific and might not always be documented as part of the mavlink specification. (uint8_t)

                '''
                return self.send(self.v2_extension_encode(target_network, target_system, target_component, message_type, payload))

        def memory_vect_encode(self, address, ver, type, value):
                '''
                Send raw controller memory. The use of this message is discouraged for
                normal packets, but a quite efficient way for testing
                new messages and getting experimental debug output.

                address                   : Starting address of the debug variables (uint16_t)
                ver                       : Version code of the type variable. 0=unknown, type ignored and assumed int16_t. 1=as below (uint8_t)
                type                      : Type code of the memory variables. for ver = 1: 0=16 x int16_t, 1=16 x uint16_t, 2=16 x Q15, 3=16 x 1Q14 (uint8_t)
                value                     : Memory contents at specified address (int8_t)

                '''
                return MAVLink_memory_vect_message(address, ver, type, value)

        def memory_vect_send(self, address, ver, type, value):
                '''
                Send raw controller memory. The use of this message is discouraged for
                normal packets, but a quite efficient way for testing
                new messages and getting experimental debug output.

                address                   : Starting address of the debug variables (uint16_t)
                ver                       : Version code of the type variable. 0=unknown, type ignored and assumed int16_t. 1=as below (uint8_t)
                type                      : Type code of the memory variables. for ver = 1: 0=16 x int16_t, 1=16 x uint16_t, 2=16 x Q15, 3=16 x 1Q14 (uint8_t)
                value                     : Memory contents at specified address (int8_t)

                '''
                return self.send(self.memory_vect_encode(address, ver, type, value))

        def debug_vect_encode(self, name, time_usec, x, y, z):
                '''
                

                name                      : Name (char)
                time_usec                 : Timestamp (uint64_t)
                x                         : x (float)
                y                         : y (float)
                z                         : z (float)

                '''
                return MAVLink_debug_vect_message(name, time_usec, x, y, z)

        def debug_vect_send(self, name, time_usec, x, y, z):
                '''
                

                name                      : Name (char)
                time_usec                 : Timestamp (uint64_t)
                x                         : x (float)
                y                         : y (float)
                z                         : z (float)

                '''
                return self.send(self.debug_vect_encode(name, time_usec, x, y, z))

        def named_value_float_encode(self, time_boot_ms, name, value):
                '''
                Send a key-value pair as float. The use of this message is discouraged
                for normal packets, but a quite efficient way for
                testing new messages and getting experimental debug
                output.

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                name                      : Name of the debug variable (char)
                value                     : Floating point value (float)

                '''
                return MAVLink_named_value_float_message(time_boot_ms, name, value)

        def named_value_float_send(self, time_boot_ms, name, value):
                '''
                Send a key-value pair as float. The use of this message is discouraged
                for normal packets, but a quite efficient way for
                testing new messages and getting experimental debug
                output.

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                name                      : Name of the debug variable (char)
                value                     : Floating point value (float)

                '''
                return self.send(self.named_value_float_encode(time_boot_ms, name, value))

        def named_value_int_encode(self, time_boot_ms, name, value):
                '''
                Send a key-value pair as integer. The use of this message is
                discouraged for normal packets, but a quite efficient
                way for testing new messages and getting experimental
                debug output.

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                name                      : Name of the debug variable (char)
                value                     : Signed integer value (int32_t)

                '''
                return MAVLink_named_value_int_message(time_boot_ms, name, value)

        def named_value_int_send(self, time_boot_ms, name, value):
                '''
                Send a key-value pair as integer. The use of this message is
                discouraged for normal packets, but a quite efficient
                way for testing new messages and getting experimental
                debug output.

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                name                      : Name of the debug variable (char)
                value                     : Signed integer value (int32_t)

                '''
                return self.send(self.named_value_int_encode(time_boot_ms, name, value))

        def statustext_encode(self, severity, text):
                '''
                Status text message. These messages are printed in yellow in the COMM
                console of QGroundControl. WARNING: They consume quite
                some bandwidth, so use only for important status and
                error messages. If implemented wisely, these messages
                are buffered on the MCU and sent only at a limited
                rate (e.g. 10 Hz).

                severity                  : Severity of status. Relies on the definitions within RFC-5424. See enum MAV_SEVERITY. (uint8_t)
                text                      : Status text message, without null termination character (char)

                '''
                return MAVLink_statustext_message(severity, text)

        def statustext_send(self, severity, text):
                '''
                Status text message. These messages are printed in yellow in the COMM
                console of QGroundControl. WARNING: They consume quite
                some bandwidth, so use only for important status and
                error messages. If implemented wisely, these messages
                are buffered on the MCU and sent only at a limited
                rate (e.g. 10 Hz).

                severity                  : Severity of status. Relies on the definitions within RFC-5424. See enum MAV_SEVERITY. (uint8_t)
                text                      : Status text message, without null termination character (char)

                '''
                return self.send(self.statustext_encode(severity, text))

        def debug_encode(self, time_boot_ms, ind, value):
                '''
                Send a debug value. The index is used to discriminate between values.
                These values show up in the plot of QGroundControl as
                DEBUG N.

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                ind                       : index of debug variable (uint8_t)
                value                     : DEBUG value (float)

                '''
                return MAVLink_debug_message(time_boot_ms, ind, value)

        def debug_send(self, time_boot_ms, ind, value):
                '''
                Send a debug value. The index is used to discriminate between values.
                These values show up in the plot of QGroundControl as
                DEBUG N.

                time_boot_ms              : Timestamp (milliseconds since system boot) (uint32_t)
                ind                       : index of debug variable (uint8_t)
                value                     : DEBUG value (float)

                '''
                return self.send(self.debug_encode(time_boot_ms, ind, value))

