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16 lines
981 B
Plaintext
16 lines
981 B
Plaintext
# Fixed Wing Longitudinal Setpoint message
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#
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# Used by the fw_lateral_longitudinal_control module
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# 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.
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# If both altitude and height_rate are NAN, the controller maintains the current altitude.
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uint32 MESSAGE_VERSION = 0
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uint64 timestamp # [us] Time since system start
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float32 altitude # [m] Altitude setpoint AMSL, not controlled directly if NAN or if height_rate is finite
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float32 height_rate # [m/s] [@frame ENU] Scalar height rate setpoint. NAN if not controlled directly
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float32 equivalent_airspeed # [m/s] [@range 0, inf] Scalar equivalent airspeed setpoint. NAN if system default should be used
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float32 pitch_direct # [rad] [@range -pi, pi] [@frame FRD] NAN if not controlled, overrides total energy controller
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float32 throttle_direct # [norm] [@range 0,1] NAN if not controlled, overrides total energy controller
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