mirror of https://github.com/ArduPilot/ardupilot
AC_AttControl: get_max_rate_step_bf_roll, pitch and yaw
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@ -715,3 +715,27 @@ float AC_AttitudeControl::sqrt_controller(float error, float p, float second_ord
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return error*p;
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}
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}
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// Maximum roll rate step size that results in maximum output after 4 time steps
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float AC_AttitudeControl::max_rate_step_bf_roll()
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{
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float alpha = _pid_rate_roll.get_filt_alpha();
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float alpha_remaining = 1-alpha;
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return AC_ATTITUDE_RATE_RP_CONTROLLER_OUT_MAX/((alpha_remaining*alpha_remaining*alpha_remaining*alpha*_pid_rate_roll.kD())/_dt + _pid_rate_roll.kP());
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}
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// Maximum pitch rate step size that results in maximum output after 4 time steps
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float AC_AttitudeControl::max_rate_step_bf_pitch()
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{
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float alpha = _pid_rate_pitch.get_filt_alpha();
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float alpha_remaining = 1-alpha;
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return AC_ATTITUDE_RATE_RP_CONTROLLER_OUT_MAX/((alpha_remaining*alpha_remaining*alpha_remaining*alpha*_pid_rate_pitch.kD())/_dt + _pid_rate_pitch.kP());
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}
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// Maximum yaw rate step size that results in maximum output after 4 time steps
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float AC_AttitudeControl::max_rate_step_bf_yaw()
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{
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float alpha = _pid_rate_yaw.get_filt_alpha();
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float alpha_remaining = 1-alpha;
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return AC_ATTITUDE_RATE_RP_CONTROLLER_OUT_MAX/((alpha_remaining*alpha_remaining*alpha_remaining*alpha*_pid_rate_yaw.kD())/_dt + _pid_rate_yaw.kP());
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}
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@ -137,6 +137,20 @@ public:
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void rate_bf_pitch_target(float rate_cds) { _rate_bf_target.y = rate_cds; }
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void rate_bf_yaw_target(float rate_cds) { _rate_bf_target.z = rate_cds; }
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// Maximum roll rate step size that results in maximum output after 4 time steps
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float max_rate_step_bf_roll();
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// Maximum pitch rate step size that results in maximum output after 4 time steps
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float max_rate_step_bf_pitch();
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// Maximum yaw rate step size that results in maximum output after 4 time steps
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float max_rate_step_bf_yaw();
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// Maximum roll step size that results in maximum output after 4 time steps
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float max_angle_step_bf_roll() { return max_rate_step_bf_roll()/_p_angle_roll.kP(); }
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// Maximum pitch step size that results in maximum output after 4 time steps
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float max_angle_step_bf_pitch() { return max_rate_step_bf_pitch()/_p_angle_pitch.kP(); }
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// Maximum yaw step size that results in maximum output after 4 time steps
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float max_angle_step_bf_yaw() { return max_rate_step_bf_yaw()/_p_angle_yaw.kP(); }
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// rate_ef_targets - returns rate controller body-frame targets (for reporting)
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const Vector3f& rate_bf_targets() const { return _rate_bf_target; }
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