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flightgear/src/Autopilot/predictor.cxx

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2.5 KiB
C++

// predictor.cxx - predict future values
//
// 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.
//
#include "predictor.hxx"
using namespace FGXMLAutopilot;
using std::endl;
using std::cout;
Predictor::Predictor () :
AnalogComponent(),
_average(0.0)
{
}
bool Predictor::configure(const string& nodeName, SGPropertyNode_ptr configNode)
{
SG_LOG( SG_AUTOPILOT, SG_BULK, "Predictor::configure(" << nodeName << ")" << endl );
if( AnalogComponent::configure( nodeName, configNode ) )
return true;
if( nodeName == "config" ) {
Component::configure( configNode );
return true;
}
if (nodeName == "seconds") {
_seconds.push_back( new InputValue( configNode, 0 ) );
return true;
}
if (nodeName == "filter-gain") {
_filter_gain.push_back( new InputValue( configNode, 0 ) );
return true;
}
SG_LOG( SG_AUTOPILOT, SG_BULK, "Predictor::configure(" << nodeName << ") [unhandled]" << endl );
return false;
}
void Predictor::update( bool firstTime, double dt )
{
double ivalue = _valueInput.get_value();
if ( firstTime ) {
_last_value = ivalue;
}
double current = (ivalue - _last_value)/dt; // calculate current error change (per second)
_average = dt < 1.0 ? ((1.0 - dt) * _average + current * dt) : current;
// calculate output with filter gain adjustment
double output = ivalue +
(1.0 - _filter_gain.get_value()) * (_average * _seconds.get_value()) +
_filter_gain.get_value() * (current * _seconds.get_value());
output = clamp( output );
set_output_value( output );
_last_value = ivalue;
}