pidfilter.h

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// -*- mode:C++; tab-width:4; c-basic-offset:4; indent-tabs-mode:nil -*-
 
/* 
* Copyright (C) 2010 RobotCub Consortium, European Commission FP6 Project IST-004370
* Author: Lorenzo Natale
* email:   lorenzo.natale@iit.it
* website: www.robotcub.org
* Permission is granted to copy, distribute, and/or modify this program
* under the terms of the GNU General Public License, version 2 or any
* later version published by the Free Software Foundation.
*
* A copy of the license can be found at
* http://www.robotcub.org/icub/license/gpl.txt
*
* This program is distributed in the hope that it will be useful, but
* WITHOUT ANY WARRANTY; without even the implied warranty of
* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General
* Public License for more details
*/
#ifndef __PidFilterh__
#define __PidFilterh__
 
#include <math.h>
 
class PidFilter  
{
private:
    double error_old;       //error at previous step
    double Kp,Kd,Ki;        //proportional, derivative and integral gains
 
    // integrative stuff
    double Umax;            //maximum value of the control
    double Sn;              //integal value
 
    //computes the pd portion of the control
    inline double pd(double error) 
    {
        double ret=Kp*error+Kd*(error-error_old);
        return ret;
    }
 
public:
    PidFilter(void);
    PidFilter(double kp, double kd=0, double ki = 0, double u = 0.0);
    PidFilter(const PidFilter& f);
    void operator=(const PidFilter& f);
    virtual ~PidFilter(void);
 
    inline void setKs(double kp, double kd=0.0, double ki=0.0, double u_max = 0.0)
    {
        Kp = kp;
        Kd = kd;
        Ki = ki;
 
        Sn = 0;
        Umax = u_max;
    }
 
    inline void reset(double error = 0.0)
    {
        Sn = 0.0;
        error_old = error;
    }
 
    // computes the PID control with anti reset wind up scheme
    inline double pid (double error)
    {
    double u_tmp;
    double Sn_tmp;
    double u_pd;
    double u;
 
    //compute the pd part
    u_pd = pd(error);
 
    //compute the temporary integral part
    Sn_tmp = Sn + Ki * error;
 
    //compute the temporary control
    u_tmp = u_pd + Sn_tmp;
 
    //if no saturation occur, then temporary works fine
    Sn = Sn_tmp;
 
    //if saturation occur, redifine integral part
    if (u_tmp > Umax)
        Sn = Umax - u_pd; 
    if (u_tmp < -Umax)
        Sn = -Umax - u_pd;
 
    //redifine error_old
    error_old = error;
 
    //compute the control
    u = Sn + u_pd;
 
    return u;
    }
 
    inline double getProportional(void) const { return Kp; }
    inline double getDerivative(void) const { return Kd; }
    inline double getIntegrative(void) const { return Ki; }
};
 
class FirstOrderLowPassFilter
{
protected:
    double fc;              // cut frequency
    double Ts;              // sample time
    double y;               // filter current output
    double yold;            // old output
    double uold;            // old input
    double a1, a2;
    double b1, b2;
 
    void computeCoeff()
    {
        double tau = 1.0/(2.0*3.1415926535897932384626433832795029*fc);
        b1 = b2 = Ts;
        a1 = 2.0*tau+Ts;
        a2 = Ts-2.0*tau;
    }
 
public:
    FirstOrderLowPassFilter(const double cutFrequency, const double sampleTime, const double y0){
        fc = cutFrequency;
        Ts = sampleTime;
        computeCoeff();
        init(y0);
    }
 
    void init(const double y0)
    {
        y = y0;
        yold = y0;
        uold = (a1+a2)/(b1+b2)*y0;
    }
 
    double getCutFrequency() { return fc; }
 
    double getSampleTime() { return Ts; }
 
    double filt(double u)
    {
        y = (b1*u + b2*uold - a2*yold) / a1;
        uold = u;
        yold = y;
        return y;
    }
 
    double output() { return y; }
};
 
#endif