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https://github.com/ArduPilot/ardupilot
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AC_PID: fixes after peer review of AC_PID_2D
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@ -4,6 +4,11 @@
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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_HZ_DEFAULT 20.0f // default input filter frequency
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#define AC_PID_2D_FILT_HZ_MIN 0.01f // minimum 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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@ -109,7 +114,7 @@ void AC_PID_2D::set_input(const Vector2f &input)
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// update filter and calculate derivative
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const Vector2f input_delta = (input - _input) * _filt_alpha;
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_input = _input + input_delta;
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_input += input_delta;
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set_input_filter_d(input_delta);
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}
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@ -117,14 +122,14 @@ void AC_PID_2D::set_input(const Vector2f &input)
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// set_input_filter_d - set input to PID controller
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// only input to the D portion of the controller is filtered
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// this should be called before any other calls to get_p, get_i or get_d
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void AC_PID_2D::set_input_filter_d(Vector2f input_delta)
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void AC_PID_2D::set_input_filter_d(const Vector2f& input_delta)
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{
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// don't process inf or NaN
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if (!isfinite(input_delta.x) && !isfinite(input_delta.y)) {
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return;
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}
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// reset input filter to value received
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// reset input filter
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if (_flags._reset_filter) {
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_flags._reset_filter = false;
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_derivative.x = 0.0f;
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@ -133,8 +138,8 @@ void AC_PID_2D::set_input_filter_d(Vector2f input_delta)
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// update filter and calculate derivative
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if (is_positive(_dt)) {
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Vector2f derivative = input_delta / _dt;
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Vector2f delta_derivative = (derivative - _derivative) * _filt_alpha_d;
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const Vector2f derivative = input_delta / _dt;
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const Vector2f delta_derivative = (derivative - _derivative) * _filt_alpha_d;
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_derivative += delta_derivative;
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}
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}
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@ -214,21 +219,6 @@ void AC_PID_2D::save_gains()
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_filt_d_hz.save();
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}
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/// Overload the function call operator to permit easy initialisation
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void AC_PID_2D::operator() (float p, float i, float imaxval, float input_filt_hz, float input_filt_d_hz, float dt)
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{
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_kp = p;
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_ki = i;
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_kd = i;
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_imax = fabsf(imaxval);
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_filt_hz = input_filt_hz;
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_filt_d_hz = input_filt_d_hz;
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_dt = dt;
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// calculate the input filter alpha
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calc_filt_alpha();
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calc_filt_alpha_d();
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}
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// calc_filt_alpha - recalculate the input filter alpha
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void AC_PID_2D::calc_filt_alpha()
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{
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@ -8,11 +8,6 @@
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#include <stdlib.h>
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#include <cmath>
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#define AC_PID_2D_FILT_HZ_DEFAULT 20.0f // default input filter frequency
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#define AC_PID_2D_FILT_HZ_MIN 0.01f // minimum 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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/// @class AC_PID_2D
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/// @brief Copter PID control class
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class AC_PID_2D {
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@ -49,9 +44,6 @@ public:
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// save gain to eeprom
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void save_gains();
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/// operator function call for easy initialisation
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void operator() (float p, float i, float imaxval, float input_filt_hz, float input_filt_D_hz, float dt);
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// get accessors
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AP_Float &kP() { return _kp; }
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AP_Float &kI() { return _ki; }
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@ -81,7 +73,7 @@ protected:
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// set_input_filter_d - set input to PID controller
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// only input to the D portion of the controller is filtered
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// this should be called before any other calls to get_p, get_i or get_d
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void set_input_filter_d(Vector2f input_delta);
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void set_input_filter_d(const Vector2f& input_delta);
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// calc_filt_alpha - recalculate the input filter alpha
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void calc_filt_alpha();
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