PX4-Autopilot/docs/uk/msg_docs/FixedWingLongitudinalSetpoint.md
PX4 Build Bot 602add3ec1
New Crowdin translations - uk (#26432)
Co-authored-by: Crowdin Bot <support+bot@crowdin.com>
2026-02-18 16:44:45 +11:00

4.0 KiB

pageClass
pageClass
is-wide-page

FixedWingLongitudinalSetpoint (UORB message)

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.

TOPICS: fixed_winglongitudinal_setpoint

Fields

Назва Тип Unit [Frame] Range/Enum Опис
timestamp uint64 time since system start (microseconds)
altitude float32 m Altitude setpoint AMSL, not controlled directly if NAN or if height_rate is finite
height_rate float32 ENU Scalar height rate setpoint. NAN if not controlled directly
equivalent_airspeed float32 m/s [0 : inf] Scalar equivalent airspeed setpoint. NAN if system default should be used
pitch_direct float32 FRD [-pi : pi] NAN if not controlled, overrides total energy controller
throttle_direct float32 norm [0 : 1] NAN if not controlled, overrides total energy controller

Constants

Назва Тип Значення Опис
MESSAGE_VERSION uint32 0

Source Message

Source file (GitHub)

:::details Click here to see original file

# 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] [@range 0, inf] Scalar equivalent airspeed setpoint. NAN if system default should be used
float32 pitch_direct 			# [rad] [@range -pi, pi] [FRD] NAN if not controlled, overrides total energy controller
float32 throttle_direct 		# [norm] [@range 0,1] NAN if not controlled, overrides total energy controller

:::