ardupilot/libraries/AC_PID/AC_P_1D.h

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#pragma once
/// @file AC_P_1D.h
/// @brief Generic P controller, with EEPROM-backed storage of constants.
#include <AP_Common/AP_Common.h>
#include <AP_Param/AP_Param.h>
/// @class AC_P_1D
/// @brief Object managing one P controller
class AC_P_1D {
public:
// constructor
AC_P_1D(float initial_p, float dt);
// set time step in seconds
void set_dt(float dt) { _dt = dt; }
// update_all - set target and measured inputs to P controller and calculate outputs
// target and measurement are filtered
// if measurement is further than error_min or error_max (see set_limits method)
// the target is moved closer to the measurement and limit_min or limit_max will be set true
float update_all(float &target, float measurement, bool &limit_min, bool &limit_max) WARN_IF_UNUSED;
// set_limits - sets the maximum error to limit output and first and second derivative of output
void set_limits(float output_min, float output_max, float D_Out_max = 0.0f, float D2_Out_max = 0.0f);
// set_error_limits - reduce maximum position error to error_max
// to be called after setting limits
void set_error_limits(float error_min, float error_max);
// get_error_min - return minimum position error
float get_error_min() const { return _error_min; }
// get_error_max - return maximum position error
float get_error_max() const { return _error_max; }
// save gain to eeprom
void save_gains() { _kp.save(); }
// accessors
AP_Float &kP() WARN_IF_UNUSED { return _kp; }
const AP_Float &kP() const WARN_IF_UNUSED { return _kp; }
float get_error() const { return _error; }
// set accessors
void kP(float v) { _kp.set(v); }
// parameter var table
static const struct AP_Param::GroupInfo var_info[];
private:
// parameters
AP_Float _kp;
// internal variables
float _dt; // time step in seconds
float _error; // time step in seconds
float _error_min; // error limit in negative direction
float _error_max; // error limit in positive direction
float _D1_max; // maximum first derivative of output
};