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synced 2026-10-15 07:33:34 +08:00
FW control: Remove unused parameters
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@@ -168,7 +168,6 @@ private:
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float p_rmax_pos;
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float p_rmax_neg;
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float p_integrator_max;
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float p_roll_feedforward;
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float r_p;
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float r_i;
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float r_ff;
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@@ -178,7 +177,6 @@ private:
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float y_i;
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float y_d;
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float y_ff;
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float y_roll_feedforward;
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float y_integrator_max;
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float y_coordinated_min_speed;
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int32_t y_coordinated_method;
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@@ -211,7 +209,6 @@ private:
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param_t p_rmax_pos;
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param_t p_rmax_neg;
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param_t p_integrator_max;
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param_t p_roll_feedforward;
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param_t r_p;
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param_t r_i;
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param_t r_ff;
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@@ -221,7 +218,6 @@ private:
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param_t y_i;
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param_t y_d;
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param_t y_ff;
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param_t y_roll_feedforward;
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param_t y_integrator_max;
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param_t y_coordinated_min_speed;
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param_t y_coordinated_method;
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@@ -374,7 +370,6 @@ FixedwingAttitudeControl::FixedwingAttitudeControl() :
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_parameter_handles.p_rmax_pos = param_find("FW_P_RMAX_POS");
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_parameter_handles.p_rmax_neg = param_find("FW_P_RMAX_NEG");
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_parameter_handles.p_integrator_max = param_find("FW_PR_IMAX");
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_parameter_handles.p_roll_feedforward = param_find("FW_P_ROLLFF");
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_parameter_handles.r_p = param_find("FW_RR_P");
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_parameter_handles.r_i = param_find("FW_RR_I");
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@@ -450,7 +445,6 @@ FixedwingAttitudeControl::parameters_update()
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param_get(_parameter_handles.p_rmax_pos, &(_parameters.p_rmax_pos));
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param_get(_parameter_handles.p_rmax_neg, &(_parameters.p_rmax_neg));
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param_get(_parameter_handles.p_integrator_max, &(_parameters.p_integrator_max));
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param_get(_parameter_handles.p_roll_feedforward, &(_parameters.p_roll_feedforward));
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param_get(_parameter_handles.r_p, &(_parameters.r_p));
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param_get(_parameter_handles.r_i, &(_parameters.r_i));
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@@ -493,7 +487,6 @@ FixedwingAttitudeControl::parameters_update()
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_pitch_ctrl.set_integrator_max(_parameters.p_integrator_max);
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_pitch_ctrl.set_max_rate_pos(math::radians(_parameters.p_rmax_pos));
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_pitch_ctrl.set_max_rate_neg(math::radians(_parameters.p_rmax_neg));
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_pitch_ctrl.set_roll_ff(_parameters.p_roll_feedforward);
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/* roll control parameters */
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_roll_ctrl.set_time_constant(_parameters.tconst);
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@@ -128,17 +128,6 @@ PARAM_DEFINE_FLOAT(FW_P_RMAX_NEG, 60.0f);
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*/
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PARAM_DEFINE_FLOAT(FW_PR_IMAX, 0.4f);
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/**
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* Roll to Pitch feedforward gain.
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*
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* This compensates during turns and ensures the nose stays level.
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*
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* @min 0.0
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* @max 2.0
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* @group FW Attitude Control
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*/
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PARAM_DEFINE_FLOAT(FW_P_ROLLFF, 0.0f);
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/**
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* Roll rate proportional Gain
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*
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