// 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; //------------------------------------------------------------------------------ Predictor::Predictor () : AnalogComponent(), _last_value(0), _average(0) { } //------------------------------------------------------------------------------ bool Predictor::configure( SGPropertyNode& cfg_node, const std::string& cfg_name, SGPropertyNode& prop_root ) { if( cfg_name == "config" ) { Component::configure(prop_root, cfg_node); return true; } if (cfg_name == "seconds") { _seconds.push_back( new InputValue(prop_root, cfg_node, 0) ); return true; } if (cfg_name == "filter-gain") { _filter_gain.push_back( new InputValue(prop_root, cfg_node, 0) ); return true; } return AnalogComponent::configure(cfg_node, cfg_name, prop_root); } //------------------------------------------------------------------------------ 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; } // Register the subsystem. SGSubsystemMgr::Registrant registrantPredictor;