forked from Archive/PX4-Autopilot
tecs_status.msg: directly add underspeed ratio to msg instead of boolean
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
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@ -26,4 +26,4 @@ float32 throttle_sp # Current throttle setpoint [-]
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float32 pitch_sp_rad # Current pitch setpoint [rad]
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float32 pitch_sp_rad # Current pitch setpoint [rad]
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float32 throttle_trim # estimated throttle value [0,1] required to fly level at equivalent_airspeed_sp in the current atmospheric conditions
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float32 throttle_trim # estimated throttle value [0,1] required to fly level at equivalent_airspeed_sp in the current atmospheric conditions
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bool underspeed_mode_enabled # System has detected a low airspeed and takes measures to avoid stalling the plane
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float32 underspeed_ratio # 0: no underspeed, 1: maximal underspeed. Controller takes measures to avoid stall proportional to ratio if >0.
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@ -646,7 +646,7 @@ public:
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float get_throttle_setpoint() {return _control.getThrottleSetpoint();}
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float get_throttle_setpoint() {return _control.getThrottleSetpoint();}
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uint64_t timestamp() { return _update_timestamp; }
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uint64_t timestamp() { return _update_timestamp; }
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bool underspeed_detected() { return _control.getRatioUndersped() > 0.f; }
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float get_underspeed_ratio() { return _control.getRatioUndersped(); }
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private:
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private:
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TECSControl _control; ///< Control submodule.
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TECSControl _control; ///< Control submodule.
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@ -506,7 +506,7 @@ FixedwingPositionControl::tecs_status_publish(float alt_sp, float equivalent_air
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tecs_status.throttle_sp = _tecs.get_throttle_setpoint();
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tecs_status.throttle_sp = _tecs.get_throttle_setpoint();
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tecs_status.pitch_sp_rad = _tecs.get_pitch_setpoint();
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tecs_status.pitch_sp_rad = _tecs.get_pitch_setpoint();
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tecs_status.throttle_trim = throttle_trim;
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tecs_status.throttle_trim = throttle_trim;
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tecs_status.underspeed_mode_enabled = _tecs.underspeed_detected();
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tecs_status.underspeed_ratio = _tecs.get_underspeed_ratio();
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tecs_status.timestamp = hrt_absolute_time();
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tecs_status.timestamp = hrt_absolute_time();
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