mirror of https://github.com/ArduPilot/ardupilot
212 lines
6.3 KiB
C++
212 lines
6.3 KiB
C++
/// @file AC_PID_2D.cpp
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/// @brief Generic PID algorithm
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#include <AP_Math/AP_Math.h>
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#include "AC_PID_2D.h"
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#define AC_PID_2D_FILT_E_HZ_DEFAULT 20.0f // default input filter frequency
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#define AC_PID_2D_FILT_D_HZ_DEFAULT 10.0f // default input filter frequency
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#define AC_PID_2D_FILT_D_HZ_MIN 0.005f // minimum input filter frequency
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const AP_Param::GroupInfo AC_PID_2D::var_info[] = {
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// @Param: P
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// @DisplayName: PID Proportional Gain
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// @Description: P Gain which produces an output value that is proportional to the current error value
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AP_GROUPINFO("P", 0, AC_PID_2D, _kp, 0),
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// @Param: I
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// @DisplayName: PID Integral Gain
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// @Description: I Gain which produces an output that is proportional to both the magnitude and the duration of the error
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AP_GROUPINFO("I", 1, AC_PID_2D, _ki, 0),
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// @Param: IMAX
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// @DisplayName: PID Integral Maximum
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// @Description: The maximum/minimum value that the I term can output
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AP_GROUPINFO("IMAX", 2, AC_PID_2D, _kimax, 0),
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// @Param: FLTE
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// @DisplayName: PID Input filter frequency in Hz
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// @Description: Input filter frequency in Hz
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// @Units: Hz
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AP_GROUPINFO("FLTE", 3, AC_PID_2D, _filt_E_hz, AC_PID_2D_FILT_E_HZ_DEFAULT),
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// @Param: D
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// @DisplayName: PID Derivative Gain
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// @Description: D Gain which produces an output that is proportional to the rate of change of the error
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AP_GROUPINFO("D", 4, AC_PID_2D, _kd, 0),
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// @Param: FLTD
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// @DisplayName: D term filter frequency in Hz
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// @Description: D term filter frequency in Hz
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// @Units: Hz
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AP_GROUPINFO("FLTD", 5, AC_PID_2D, _filt_D_hz, AC_PID_2D_FILT_D_HZ_DEFAULT),
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// @Param: FF
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// @DisplayName: PID Feed Forward Gain
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// @Description: FF Gain which produces an output that is proportional to the magnitude of the target
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AP_GROUPINFO("FF", 6, AC_PID_2D, _kff, 0),
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AP_GROUPEND
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};
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// Constructor
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AC_PID_2D::AC_PID_2D(float initial_kP, float initial_kI, float initial_kD, float initial_kFF, float initial_imax, float initial_filt_E_hz, float initial_filt_D_hz, float dt) :
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_dt(dt)
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{
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// load parameter values from eeprom
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AP_Param::setup_object_defaults(this, var_info);
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_kp = initial_kP;
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_ki = initial_kI;
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_kd = initial_kD;
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_kff = initial_kFF;
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_kimax = fabsf(initial_imax);
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filt_E_hz(initial_filt_E_hz);
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filt_D_hz(initial_filt_D_hz);
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// reset input filter to first value received
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_reset_filter = true;
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}
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// update_all - set target and measured inputs to PID controller and calculate outputs
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// target and error are filtered
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// the derivative is then calculated and filtered
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// the integral is then updated if it does not increase in the direction of the limit vector
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Vector2f AC_PID_2D::update_all(const Vector2f &target, const Vector2f &measurement, const Vector2f &limit)
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{
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// don't process inf or NaN
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if (target.is_nan() || target.is_inf() ||
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measurement.is_nan() || measurement.is_inf()) {
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return Vector2f{};
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}
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_target = target;
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// reset input filter to value received
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if (_reset_filter) {
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_reset_filter = false;
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_error = _target - measurement;
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_derivative.zero();
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} else {
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Vector2f error_last{_error};
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_error += ((_target - measurement) - _error) * get_filt_E_alpha();
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// calculate and filter derivative
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if (_dt > 0.0f) {
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const Vector2f derivative{(_error - error_last) / _dt};
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_derivative += (derivative - _derivative) * get_filt_D_alpha();
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}
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}
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// update I term
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update_i(limit);
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_pid_info_x.target = _target.x;
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_pid_info_x.actual = measurement.x;
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_pid_info_x.error = _error.x;
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_pid_info_x.P = _error.x * _kp;
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_pid_info_x.I = _integrator.x;
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_pid_info_x.D = _derivative.x * _kd;
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_pid_info_x.FF = _target.x * _kff;
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_pid_info_y.target = _target.y;
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_pid_info_y.actual = measurement.y;
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_pid_info_y.error = _error.y;
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_pid_info_y.P = _error.y * _kp;
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_pid_info_y.I = _integrator.y;
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_pid_info_y.D = _derivative.y * _kd;
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_pid_info_y.FF = _target.y * _kff;
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return _error * _kp + _integrator + _derivative * _kd + _target * _kff;
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}
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Vector2f AC_PID_2D::update_all(const Vector3f &target, const Vector3f &measurement, const Vector3f &limit)
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{
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return update_all(Vector2f{target.x, target.y}, Vector2f{measurement.x, measurement.y}, Vector2f{limit.x, limit.y});
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}
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// update_i - update the integral
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// If the limit is set the integral is only allowed to reduce in the direction of the limit
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void AC_PID_2D::update_i(const Vector2f &limit)
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{
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_pid_info_x.limit = false;
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_pid_info_y.limit = false;
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Vector2f delta_integrator = (_error * _ki) * _dt;
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float integrator_length = _integrator.length();
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_integrator += delta_integrator;
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// do not let integrator increase in length if delta_integrator is in the direction of limit
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if (is_positive(delta_integrator * limit) && _integrator.limit_length(integrator_length)) {
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_pid_info_x.limit = true;
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_pid_info_y.limit = true;
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}
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_integrator.limit_length(_kimax);
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}
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Vector2f AC_PID_2D::get_p() const
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{
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return _error * _kp;
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}
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const Vector2f& AC_PID_2D::get_i() const
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{
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return _integrator;
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}
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Vector2f AC_PID_2D::get_d() const
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{
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return _derivative * _kd;
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}
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Vector2f AC_PID_2D::get_ff()
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{
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_pid_info_x.FF = _target.x * _kff;
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_pid_info_y.FF = _target.y * _kff;
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return _target * _kff;
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}
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// save_gains - save gains to eeprom
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void AC_PID_2D::save_gains()
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{
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_kp.save();
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_ki.save();
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_kd.save();
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_kff.save();
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_kimax.save();
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_filt_E_hz.save();
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_filt_D_hz.save();
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}
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// get the target filter alpha
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float AC_PID_2D::get_filt_E_alpha() const
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{
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return calc_lowpass_alpha_dt(_dt, _filt_E_hz);
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}
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// get the derivative filter alpha
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float AC_PID_2D::get_filt_D_alpha() const
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{
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return calc_lowpass_alpha_dt(_dt, _filt_D_hz);
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}
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void AC_PID_2D::set_integrator(const Vector2f& target, const Vector2f& measurement, const Vector2f& i)
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{
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set_integrator(target - measurement, i);
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}
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void AC_PID_2D::set_integrator(const Vector2f& error, const Vector2f& i)
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{
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set_integrator(i - error * _kp);
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}
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void AC_PID_2D::set_integrator(const Vector2f& i)
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{
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_integrator = i;
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const float integrator_length = _integrator.length();
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if (integrator_length > _kimax) {
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_integrator *= (_kimax / integrator_length);
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}
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}
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