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flightgear/src/Autopilot/pidcontroller.hxx
Torsten Dreyer d558b52cb6 New autopilot subsystem implementation.
Split the former single-file-implementation in xmlauto.?xx into multiple
files and use some OO techniques. Started with documentation to be used
with doxygen.
2010-06-24 17:09:33 +02:00

74 lines
2.6 KiB
C++

// pidcontroller.hxx - implementation of PID controller
//
// Written by Torsten Dreyer
// Based heavily on work created by Curtis Olson, started January 2004.
//
// Copyright (C) 2004 Curtis L. Olson - http://www.flightgear.org/~curt
// Copyright (C) 2010 Torsten Dreyer - Torsten (at) t3r (dot) de
//
// This program is free software; you can redistribute it and/or
// modify it under the terms of the GNU General Public License as
// published by the Free Software Foundation; either version 2 of the
// License, or (at your option) any later version.
//
// 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.
//
// You should have received a copy of the GNU General Public License
// along with this program; if not, write to the Free Software
// Foundation, Inc., 51 Franklin Street, Fifth Floor, Boston, MA 02110-1301, USA.
//
#ifndef __PIDCONTROLLER_HXX
#define __PIDCONTROLLER_HXX 1
#ifdef HAVE_CONFIG_H
# include <config.h>
#endif
#include "analogcomponent.hxx"
#include <simgear/props/props.hxx>
#include <simgear/structure/subsystem_mgr.hxx>
namespace FGXMLAutopilot {
/**
* Roy Ovesen's PID controller
*/
class PIDController : public AnalogComponent {
private:
// Configuration values
InputValueList Kp; // proportional gain
InputValueList Ti; // Integrator time (sec)
InputValueList Td; // Derivator time (sec)
double alpha; // low pass filter weighing factor (usually 0.1)
double beta; // process value weighing factor for
// calculating proportional error
// (usually 1.0)
double gamma; // process value weighing factor for
// calculating derivative error
// (usually 0.0)
// Previous state tracking values
double ep_n_1; // ep[n-1] (prop error)
double edf_n_1; // edf[n-1] (derivative error)
double edf_n_2; // edf[n-2] (derivative error)
double u_n_1; // u[n-1] (output)
double desiredTs; // desired sampling interval (sec)
double elapsedTime; // elapsed time (sec)
protected:
bool configure( const std::string & nodeName, SGPropertyNode_ptr configNode);
public:
PIDController();
~PIDController() {}
void update( bool firstTime, double dt );
};
}
#endif // __PIDCONTROLLER_HXX