# If you change the order, add or remove arming_state_t states make sure to update the arrays # in state_machine_helper.cpp as well. uint64 timestamp # time since system start (microseconds) uint8 ARMING_STATE_INIT = 0 uint8 ARMING_STATE_STANDBY = 1 uint8 ARMING_STATE_ARMED = 2 uint8 ARMING_STATE_STANDBY_ERROR = 3 uint8 ARMING_STATE_SHUTDOWN = 4 uint8 ARMING_STATE_IN_AIR_RESTORE = 5 uint8 ARMING_STATE_MAX = 6 # FailureDetector status uint8 FAILURE_NONE = 0 uint8 FAILURE_ROLL = 1 # (1 << 0) uint8 FAILURE_PITCH = 2 # (1 << 1) uint8 FAILURE_ALT = 4 # (1 << 2) uint8 FAILURE_EXT = 8 # (1 << 3) uint8 FAILURE_ARM_ESC = 16 # (1 << 4) # HIL uint8 HIL_STATE_OFF = 0 uint8 HIL_STATE_ON = 1 # Navigation state, i.e. "what should vehicle do". uint8 NAVIGATION_STATE_MANUAL = 0 # Manual mode uint8 NAVIGATION_STATE_ALTCTL = 1 # Altitude control mode uint8 NAVIGATION_STATE_POSCTL = 2 # Position control mode uint8 NAVIGATION_STATE_AUTO_MISSION = 3 # Auto mission mode uint8 NAVIGATION_STATE_AUTO_LOITER = 4 # Auto loiter mode uint8 NAVIGATION_STATE_AUTO_RTL = 5 # Auto return to launch mode uint8 NAVIGATION_STATE_AUTO_LANDENGFAIL = 8 # Auto land on engine failure uint8 NAVIGATION_STATE_AUTO_LANDGPSFAIL = 9 # Auto land on gps failure (e.g. open loop loiter down) uint8 NAVIGATION_STATE_ACRO = 10 # Acro mode uint8 NAVIGATION_STATE_UNUSED = 11 # Free slot uint8 NAVIGATION_STATE_DESCEND = 12 # Descend mode (no position control) uint8 NAVIGATION_STATE_TERMINATION = 13 # Termination mode uint8 NAVIGATION_STATE_OFFBOARD = 14 uint8 NAVIGATION_STATE_STAB = 15 # Stabilized mode uint8 NAVIGATION_STATE_UNUSED2 = 16 # Free slot uint8 NAVIGATION_STATE_AUTO_TAKEOFF = 17 # Takeoff uint8 NAVIGATION_STATE_AUTO_LAND = 18 # Land uint8 NAVIGATION_STATE_AUTO_FOLLOW_TARGET = 19 # Auto Follow uint8 NAVIGATION_STATE_AUTO_PRECLAND = 20 # Precision land with landing target uint8 NAVIGATION_STATE_ORBIT = 21 # Orbit in a circle uint8 NAVIGATION_STATE_MAX = 22 uint8 RC_IN_MODE_DEFAULT = 0 uint8 RC_IN_MODE_OFF = 1 uint8 RC_IN_MODE_GENERATED = 2 uint8 VEHICLE_TYPE_UNKNOWN = 0 uint8 VEHICLE_TYPE_ROTARY_WING = 1 uint8 VEHICLE_TYPE_FIXED_WING = 2 uint8 VEHICLE_TYPE_ROVER = 3 uint8 VEHICLE_TYPE_AIRSHIP = 4 # state machine / state of vehicle. # Encodes the complete system state and is set by the commander app. uint8 nav_state # set navigation state machine to specified value uint64 nav_state_timestamp # time when current nav_state activated uint8 arming_state # current arming state uint8 hil_state # current hil state bool failsafe # true if system is in failsafe state (e.g.:RTL, Hover, Terminate, ...) uint64 failsafe_timestamp # time when failsafe was activated uint8 system_type # system type, contains mavlink MAV_TYPE uint8 system_id # system id, contains MAVLink's system ID field uint8 component_id # subsystem / component id, contains MAVLink's component ID field uint8 vehicle_type # Type of vehicle (fixed-wing, rotary wing, ground) # If the vehicle is a VTOL, then this value will be VEHICLE_TYPE_ROTARY_WING while flying as a multicopter, # and VEHICLE_TYPE_FIXED_WING when flying as a fixed-wing bool is_vtol # True if the system is VTOL capable bool is_vtol_tailsitter # True if the system performs a 90° pitch down rotation during transition from MC to FW bool vtol_fw_permanent_stab # True if VTOL should stabilize attitude for fw in manual mode bool in_transition_mode # True if VTOL is doing a transition bool in_transition_to_fw # True if VTOL is doing a transition from MC to FW bool rc_signal_lost # true if RC reception lost uint8 rc_input_mode # set to 1 to disable the RC input, 2 to enable manual control to RC in mapping. bool data_link_lost # datalink to GCS lost uint8 data_link_lost_counter # counts unique data link lost events bool high_latency_data_link_lost # Set to true if the high latency data link (eg. RockBlock Iridium 9603 telemetry module) is lost bool engine_failure # Set to true if an engine failure is detected bool mission_failure # Set to true if mission could not continue/finish bool geofence_violated uint8 failure_detector_status # Bitmask containing FailureDetector status [0, 0, 0, 0, 0, FAILURE_ALT, FAILURE_PITCH, FAILURE_ROLL] # see SYS_STATUS mavlink message for the following uint32 onboard_control_sensors_present uint32 onboard_control_sensors_enabled uint32 onboard_control_sensors_health uint8 ARM_DISARM_REASON_TRANSITION_TO_STANDBY = 0 uint8 ARM_DISARM_REASON_RC_STICK = 1 uint8 ARM_DISARM_REASON_RC_SWITCH = 2 uint8 ARM_DISARM_REASON_COMMAND_INTERNAL = 3 uint8 ARM_DISARM_REASON_COMMAND_EXTERNAL = 4 uint8 ARM_DISARM_REASON_MISSION_START = 5 uint8 ARM_DISARM_REASON_SAFETY_BUTTON = 6 uint8 ARM_DISARM_REASON_AUTO_DISARM_LAND = 7 uint8 ARM_DISARM_REASON_AUTO_DISARM_PREFLIGHT = 8 uint8 ARM_DISARM_REASON_KILL_SWITCH = 9 uint8 ARM_DISARM_REASON_LOCKDOWN = 10 uint8 ARM_DISARM_REASON_FAILURE_DETECTOR = 11 uint8 ARM_DISARM_REASON_SHUTDOWN = 12 uint8 ARM_DISARM_REASON_UNIT_TEST = 13 uint8 latest_arming_reason uint8 latest_disarming_reason uint64 armed_time # Arming timestamp (microseconds) uint64 takeoff_time # Takeoff timestamp (microseconds)