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flightgear/JSBsim/FGEngine.cpp

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/*******************************************************************************
Module: FGEngine.cpp
Author: Jon Berndt
Date started: 01/21/99
Called by: FGAircraft
------------- Copyright (C) 1999 Jon S. Berndt (jsb@hal-pc.org) -------------
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., 59 Temple
Place - Suite 330, Boston, MA 02111-1307, USA.
Further information about the GNU General Public License can also be found on
the world wide web at http://www.gnu.org.
FUNCTIONAL DESCRIPTION
--------------------------------------------------------------------------------
See header file.
HISTORY
--------------------------------------------------------------------------------
01/21/99 JSB Created
********************************************************************************
INCLUDES
*******************************************************************************/
#include <fstream.h>
#include <stdio.h>
#include <stdlib.h>
#include <string.h>
#include "FGEngine.h"
#include "FGState.h"
#include "FGFDMExec.h"
#include "FGAtmosphere.h"
#include "FGFCS.h"
#include "FGAircraft.h"
#include "FGTranslation.h"
#include "FGRotation.h"
#include "FGPosition.h"
#include "FGAuxiliary.h"
#include "FGOutput.h"
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/*******************************************************************************
************************************ CODE **************************************
*******************************************************************************/
FGEngine::FGEngine(FGFDMExec* fdex, char *engineName, int num)
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{
char fullpath[256];
char tag[256];
FDMExec = fdex;
State = FDMExec->GetState();
Atmosphere = FDMExec->GetAtmosphere();
FCS = FDMExec->GetFCS();
Aircraft = FDMExec->GetAircraft();
Translation = FDMExec->GetTranslation();
Rotation = FDMExec->GetRotation();
Position = FDMExec->GetPosition();
Auxiliary = FDMExec->GetAuxiliary();
Output = FDMExec->GetOutput();
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strcpy(Name, engineName);
sprintf(fullpath,"/h/curt/projects/FlightGear/Simulator/FDM/JSBsim/engine/%s.dat", engineName);
ifstream enginefile(fullpath);
if (enginefile) {
enginefile >> tag;
if (strstr(tag,"ROCKET")) Type = 0;
else if (strstr(tag,"PISTON")) Type = 1;
else if (strstr(tag,"TURBOPROP")) Type = 2;
else if (strstr(tag,"TURBOJET")) Type = 3;
else Type = 0;
enginefile >> X;
enginefile >> Y;
enginefile >> Z;
enginefile >> SLThrustMax;
enginefile >> VacThrustMax;
enginefile >> MaxThrottle;
enginefile >> MinThrottle;
enginefile >> SLFuelFlowMax;
if (Type == 0)
enginefile >> SLOxiFlowMax;
enginefile.close();
} else {
cerr << "Unable to open engine definition file " << engineName << endl;
}
EngineNumber = num;
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Thrust = 0.0;
Starved = Flameout = false;
}
FGEngine::~FGEngine(void)
{
}
float FGEngine::CalcRocketThrust(void)
{
float lastThrust;
Throttle = FCS->GetThrottle(EngineNumber);
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lastThrust = Thrust; // last actual thrust
if (Throttle < MinThrottle || Starved) {
PctPower = Thrust = 0.0; // desired thrust
Flameout = true;
} else {
PctPower = Throttle / MaxThrottle;
Thrust = PctPower*((1.0 - Atmosphere->Getrho() / 0.002378)*(VacThrustMax - SLThrustMax) +
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SLThrustMax); // desired thrust
Flameout = false;
}
Thrust += 0.8*(Thrust - lastThrust); // actual thrust
return Thrust;
}
float FGEngine::CalcPistonThrust(void)
{
return Thrust;
}
float FGEngine::CalcThrust(void)
{
switch(Type) {
case 0: // Rocket
return CalcRocketThrust();
// break;
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case 1: // Piston
return CalcPistonThrust();
// break;
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default:
return 9999.0;
// break;
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}
}
float FGEngine::CalcFuelNeed() {
FuelNeed = SLFuelFlowMax*PctPower;
return FuelNeed;
}
float FGEngine::CalcOxidizerNeed() {
OxidizerNeed = SLOxiFlowMax*PctPower;
return OxidizerNeed;
}