2016-02-24 06:27:00 -04:00
|
|
|
# VEHICLE_VTOL_STATE, should match 1:1 MAVLinks's MAV_VTOL_STATE
|
|
|
|
|
uint8 VEHICLE_VTOL_STATE_UNDEFINED = 0
|
|
|
|
|
uint8 VEHICLE_VTOL_STATE_TRANSITION_TO_FW = 1
|
|
|
|
|
uint8 VEHICLE_VTOL_STATE_TRANSITION_TO_MC = 2
|
|
|
|
|
uint8 VEHICLE_VTOL_STATE_MC = 3
|
|
|
|
|
uint8 VEHICLE_VTOL_STATE_FW = 4
|
2016-12-25 12:02:42 -04:00
|
|
|
uint8 VEHICLE_VTOL_STATE_EXTERNAL = 5
|
2016-02-24 06:27:00 -04:00
|
|
|
|
2016-02-05 08:06:51 -04:00
|
|
|
bool vtol_in_rw_mode # true: vtol vehicle is in rotating wing mode
|
2015-08-07 11:43:16 -03:00
|
|
|
bool vtol_in_trans_mode
|
2016-05-26 02:06:06 -03:00
|
|
|
bool in_transition_to_fw # True if VTOL is doing a transition from MC to FW
|
2016-02-05 08:06:51 -04:00
|
|
|
bool vtol_transition_failsafe # vtol in transition failsafe mode
|
|
|
|
|
bool fw_permanent_stab # In fw mode stabilize attitude even if in manual mode
|
|
|
|
|
float32 airspeed_tot # Estimated airspeed over control surfaces
|
