ardupilot/libraries/AC_PID/AC_P_1D.cpp

Ignoring revisions in .git-blame-ignore-revs. Click here to bypass and see the normal blame view.

88 lines
2.7 KiB
C++
Raw Permalink Normal View History

/// @file AC_P_1D.cpp
/// @brief Generic P algorithm
#include <AP_Math/AP_Math.h>
#include "AC_P_1D.h"
const AP_Param::GroupInfo AC_P_1D::var_info[] = {
// @Param: P
// @DisplayName: P Proportional Gain
// @Description: P Gain which produces an output value that is proportional to the current error value
2023-01-03 13:22:36 -04:00
AP_GROUPINFO_FLAGS_DEFAULT_POINTER("P", 0, AC_P_1D, _kp, default_kp),
AP_GROUPEND
};
// Constructor
2023-01-03 13:22:36 -04:00
AC_P_1D::AC_P_1D(float initial_p) :
default_kp(initial_p)
{
// load parameter values from eeprom
AP_Param::setup_object_defaults(this, var_info);
}
// update_all - set target and measured inputs to P controller and calculate outputs
// target and measurement are filtered
float AC_P_1D::update_all(float &target, float measurement)
{
// calculate distance _error
_error = target - measurement;
if (is_negative(_error_min) && (_error < _error_min)) {
_error = _error_min;
target = measurement + _error;
} else if (is_positive(_error_max) && (_error > _error_max)) {
_error = _error_max;
target = measurement + _error;
}
// MIN(_Dxy_max, _D2xy_max / _kxy_P) limits the max accel to the point where max jerk is exceeded
2022-12-02 08:34:53 -04:00
return sqrt_controller(_error, _kp, _D1_max, 0.0);
}
// set_limits - sets the maximum error to limit output and first and second derivative of output
// when using for a position controller, lim_err will be position error, lim_out will be correction velocity, lim_D will be acceleration, lim_D2 will be jerk
void AC_P_1D::set_limits(float output_min, float output_max, float D_Out_max, float D2_Out_max)
{
_D1_max = 0.0f;
_error_min = 0.0f;
_error_max = 0.0f;
if (is_positive(D_Out_max)) {
_D1_max = D_Out_max;
}
if (is_positive(D2_Out_max) && is_positive(_kp)) {
// limit the first derivative so as not to exceed the second derivative
_D1_max = MIN(_D1_max, D2_Out_max / _kp);
}
if (is_negative(output_min) && is_positive(_kp)) {
_error_min = inv_sqrt_controller(output_min, _kp, _D1_max);
}
if (is_positive(output_max) && is_positive(_kp)) {
_error_max = inv_sqrt_controller(output_max, _kp, _D1_max);
}
}
2021-05-19 11:10:14 -03:00
// set_error_limits - reduce maximum error to error_max
// to be called after setting limits
void AC_P_1D::set_error_limits(float error_min, float error_max)
{
if (is_negative(error_min)) {
if (!is_zero(_error_min)) {
_error_min = MAX(_error_min, error_min);
} else {
_error_min = error_min;
}
}
if (is_positive(error_max)) {
if (!is_zero(_error_max)) {
_error_max = MIN(_error_max, error_max);
} else {
_error_max = error_max;
}
}
}