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https://github.com/ArduPilot/ardupilot
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AP_TECS: add TECS_LAND_TDAMP for land damp
+ // @Description: This is the damping gain for the throttle demand loop during and auto-landing. Same as TECS_THR_DAMP but only in effect during an auto-land. Increase to add damping to correct for oscillations in speed and height. When set to 0 landing throttle damp is controlled by TECS_THR_DAMP.
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@ -202,6 +202,14 @@ const AP_Param::GroupInfo AP_TECS::var_info[] = {
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// @User: Advanced
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AP_GROUPINFO("LAND_SRC", 22, AP_TECS, _land_sink_rate_change, 0),
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// @Param: LAND_TDAMP
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// @DisplayName: Controller throttle damping when landing
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// @Description: This is the damping gain for the throttle demand loop during and auto-landing. Same as TECS_THR_DAMP but only in effect during an auto-land. Increase to add damping to correct for oscillations in speed and height. When set to 0 landing throttle damp is controlled by TECS_THR_DAMP.
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// @Range: 0.1 1.0
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// @Increment: 0.1
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// @User: Advanced
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AP_GROUPINFO("LAND_TDAMP", 23, AP_TECS, _land_throttle_damp, 0),
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AP_GROUPEND
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};
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@ -586,7 +594,11 @@ void AP_TECS::_update_throttle(void)
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ff_throttle = nomThr + STEdot_dem / (_STEdot_max - _STEdot_min) * (_THRmaxf - _THRminf);
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// Calculate PD + FF throttle
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_throttle_dem = (_STE_error + STEdot_error * _thrDamp) * K_STE2Thr + ff_throttle;
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float throttle_damp = _thrDamp;
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if (_is_doing_auto_land && !is_zero(_land_throttle_damp)) {
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throttle_damp = _land_throttle_damp;
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}
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_throttle_dem = (_STE_error + STEdot_error * throttle_damp) * K_STE2Thr + ff_throttle;
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// Constrain throttle demand
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_throttle_dem = constrain_float(_throttle_dem, _THRminf, _THRmaxf);
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@ -150,6 +150,7 @@ private:
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AP_Float _ptchDamp;
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AP_Float _landDamp;
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AP_Float _thrDamp;
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AP_Float _land_throttle_damp;
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AP_Float _integGain;
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AP_Float _vertAccLim;
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AP_Float _rollComp;
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