333c790086
Added <startup-current> param. Default is false which preserves previous behaviour where internal state is initialised to zero. Otherwise we initialise internal state using the current error value, which can reduce oscillations. Added <startup-its> param, default is zero. For the first <startup-its> iterations we don't update the output, which can be used to cope with initial bad data from earlier controllers. Also refactored the code to hopefully make it clearer and modified debug logging to output all info in a single statement and on a single line for clarity. For example avoid initial oscillations with: <pid-controller> .. <startup-current>true</startup-current> ... </pid-controller>
93 lines
3.2 KiB
C++
93 lines
3.2 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)
|
|
|
|
/* If startup_current is false (the default), we initialise internal state
|
|
variables to zero.
|
|
|
|
Otherwise we initialise internal variables to the current values, which can
|
|
reduce initial transient behaviour. */
|
|
bool startup_current;
|
|
|
|
/* For the first startup_its iterations we don't modify our output. Default
|
|
is zero. */
|
|
unsigned startup_its;
|
|
|
|
unsigned iteration;
|
|
|
|
protected:
|
|
virtual bool configure( SGPropertyNode& cfg_node,
|
|
const std::string& cfg_name,
|
|
SGPropertyNode& prop_root );
|
|
|
|
public:
|
|
PIDController();
|
|
~PIDController() {}
|
|
|
|
// Subsystem identification.
|
|
static const char* staticSubsystemClassId() { return "pid-controller"; }
|
|
|
|
void update( bool firstTime, double dt );
|
|
};
|
|
|
|
}
|
|
#endif // __PIDCONTROLLER_HXX
|