forked from Archive/PX4-Autopilot
add new parameters for roll and pitch angular rate limits
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@ -202,7 +202,7 @@ private:
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float roll_rate_max;
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float pitch_rate_max;
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float yaw_rate_max;
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math::Vector<3> mc_rate_max; /**< attitude rate limits in stabilized modes */
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math::Vector<3> mc_rate_max; /**< attitude rate limits in all modes */
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float man_roll_max;
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float man_pitch_max;
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@ -656,14 +656,11 @@ MulticopterAttitudeControl::control_attitude(float dt)
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/* calculate angular rates setpoint */
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_rates_sp = _params.att_p.emult(e_R);
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/* limit roll and pitch rates */
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for (int i = 0; i < 2; i++) {
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_rates_sp(i) = math::constrain(_rates_sp(i), -_params.acro_rate_max(i), _params.acro_rate_max(i));
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/* limit rates */
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for (int i = 0; i < 3; i++) {
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_rates_sp(i) = math::constrain(_rates_sp(i), -_params.mc_rate_max(i), _params.mc_rate_max(i));
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}
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/* limit yaw rate */
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_rates_sp(2) = math::constrain(_rates_sp(2), -_params.yaw_rate_max, _params.yaw_rate_max);
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/* feed forward yaw setpoint rate */
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_rates_sp(2) += _v_att_sp.yaw_sp_move_rate * yaw_w * _params.yaw_ff;
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}
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@ -215,7 +215,7 @@ PARAM_DEFINE_FLOAT(MC_YAW_FF, 0.5f);
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* @max 360.0
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* @group Multicopter Attitude Control
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*/
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PARAM_DEFINE_FLOAT(MC_ROLLRATE_MAX, 360.0f);
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PARAM_DEFINE_FLOAT(MC_ROLLRATE_MAX, 120.0f);
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/**
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* Max pitch rate
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@ -227,7 +227,7 @@ PARAM_DEFINE_FLOAT(MC_ROLLRATE_MAX, 360.0f);
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* @max 360.0
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* @group Multicopter Attitude Control
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*/
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PARAM_DEFINE_FLOAT(MC_PITCHRATE_MAX, 360.0f);
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PARAM_DEFINE_FLOAT(MC_PITCHRATE_MAX, 120.0f);
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/**
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* Max yaw rate
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