PX4-Autopilot/msg/versioned/FixedWingLongitudinalSetpoint.msg

15 lines
984 B
Plaintext

# Fixed Wing Longitudinal Setpoint message
# Used by the fw_lateral_longitudinal_control module
# If pitch_direct and throttle_direct are not both finite, then the controller relies on altitude/height_rate and equivalent_airspeed to control vertical motion.
# If both altitude and height_rate are NAN, the controller maintains the current altitude.
uint32 MESSAGE_VERSION = 0
uint64 timestamp # time since system start (microseconds)
float32 altitude # [m] Altitude setpoint AMSL, not controlled directly if NAN or if height_rate is finite
float32 height_rate # [m/s] [ENU] Scalar height rate setpoint. NAN if not controlled directly
float32 equivalent_airspeed # [m/s] [0, inf] Scalar equivalent airspeed setpoint. NAN if system default should be used
float32 pitch_direct # [rad] [-pi, pi] [FRD] NAN if not controlled, overrides total energy controller
float32 throttle_direct # [0,1] NAN if not controlled, overrides total energy controller