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Ability to disable airspeed scaling (#14334)
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@@ -263,7 +263,8 @@ float FixedwingAttitudeControl::get_airspeed_and_update_scaling()
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* Forcing the scaling to this value allows reasonable handheld tests.
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*/
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const float airspeed_constrained = constrain(airspeed, _param_fw_airspd_min.get(), _param_fw_airspd_max.get());
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_airspeed_scaling = _param_fw_airspd_trim.get() / airspeed_constrained;
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_airspeed_scaling = (_param_fw_arsp_scale_en.get()) ? (_param_fw_airspd_trim.get() / airspeed_constrained) : 1.0f;
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return airspeed;
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}
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@@ -149,6 +149,8 @@ private:
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(ParamFloat<px4::params::FW_AIRSPD_TRIM>) _param_fw_airspd_trim,
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(ParamInt<px4::params::FW_ARSP_MODE>) _param_fw_arsp_mode,
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(ParamInt<px4::params::FW_ARSP_SCALE_EN>) _param_fw_arsp_scale_en,
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(ParamBool<px4::params::FW_BAT_SCALE_EN>) _param_fw_bat_scale_en,
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(ParamFloat<px4::params::FW_DTRIM_P_FLPS>) _param_fw_dtrim_p_flps,
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@@ -537,6 +537,21 @@ PARAM_DEFINE_FLOAT(FW_FLAPERON_SCL, 0.0f);
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*/
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PARAM_DEFINE_INT32(FW_ARSP_MODE, 0);
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/**
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* Enable airspeed scaling
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*
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* This enables a logic that automatically adjusts the output of the rate controller to take
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* into account the real torque produced by an aerodynamic control surface given
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* the current deviation from the trim airspeed (FW_AIRSPD_TRIM).
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*
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* Enable when using aerodynamic control surfaces (e.g.: plane)
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* Disable when using rotor wings (e.g.: autogyro)
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*
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* @boolean
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* @group FW Attitude Control
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*/
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PARAM_DEFINE_INT32(FW_ARSP_SCALE_EN, 1);
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/**
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* Manual roll scale
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*
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