PX4-Autopilot/msg/vehicle_status.msg
acfloria 634697946a Add switch logic for high latency telemetry in commander
Switch to the high latency telemetry, if available, if every low latency link is lost. Switch back if any low latency link is regained. Only indicate that all links are lost if all high and low latency links are lost. Allow different timeouts for high and low latency links.
2018-04-11 15:15:28 +02:00

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# 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.
uint8 ARMING_STATE_INIT = 0
uint8 ARMING_STATE_STANDBY = 1
uint8 ARMING_STATE_ARMED = 2
uint8 ARMING_STATE_STANDBY_ERROR = 3
uint8 ARMING_STATE_REBOOT = 4
uint8 ARMING_STATE_IN_AIR_RESTORE = 5
uint8 ARMING_STATE_MAX = 6
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_RCRECOVER = 6 # RC recover mode
uint8 NAVIGATION_STATE_AUTO_RTGS = 7 # Auto return to groundstation on data link loss
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_RATTITUDE = 16 # Rattitude (aka "flip") mode
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_MAX = 21
uint8 RC_IN_MODE_DEFAULT = 0
uint8 RC_IN_MODE_OFF = 1
uint8 RC_IN_MODE_GENERATED = 2
# 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
uint8 arming_state # current arming state
uint8 hil_state # current hil state
bool failsafe # true if system is in failsafe state
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
bool is_rotary_wing # True if system is in rotary wing configuration, so for a VTOL this is only true while flying as a multicopter
bool is_vtol # True if the system is VTOL capable
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
bool high_latency_data_link_active # all low latency datalinks to GCS lost
uint8 data_link_lost_counter # counts unique data link lost events
bool engine_failure # Set to true if an engine failure is detected
bool mission_failure # Set to true if mission could not continue/finish
# see SYS_STATUS mavlink message for the following
uint32 onboard_control_sensors_present
uint32 onboard_control_sensors_enabled
uint32 onboard_control_sensors_health