2001-11-09 04:38:53 +00:00
|
|
|
/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
|
|
|
|
|
|
|
|
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
|
|
|
|
09/03/99 JSB Changed Rocket thrust equation to correct -= Thrust instead of
|
|
|
|
+= Thrust (thanks to Tony Peden)
|
|
|
|
|
|
|
|
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
|
|
|
|
INCLUDES
|
|
|
|
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
|
|
|
|
|
|
|
|
#ifdef FGFS
|
|
|
|
# include <simgear/compiler.h>
|
|
|
|
# ifdef SG_HAVE_STD_INCLUDES
|
|
|
|
# include <fstream>
|
|
|
|
# else
|
|
|
|
# include <fstream.h>
|
|
|
|
# endif
|
|
|
|
#else
|
|
|
|
# if defined(sgi) && !defined(__GNUC__)
|
|
|
|
# include <fstream.h>
|
|
|
|
# else
|
|
|
|
# include <fstream>
|
|
|
|
# endif
|
|
|
|
#endif
|
|
|
|
|
|
|
|
#include "FGEngine.h"
|
|
|
|
#include "FGTank.h"
|
|
|
|
|
|
|
|
static const char *IdSrc = "$Id$";
|
|
|
|
static const char *IdHdr = ID_ENGINE;
|
|
|
|
|
|
|
|
/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
|
|
|
|
CLASS IMPLEMENTATION
|
|
|
|
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
|
|
|
|
|
|
|
|
|
2001-11-30 17:49:37 +00:00
|
|
|
FGEngine::FGEngine(FGFDMExec* exec)
|
|
|
|
{
|
2001-11-09 04:38:53 +00:00
|
|
|
FDMExec = exec;
|
|
|
|
State = FDMExec->GetState();
|
|
|
|
Atmosphere = FDMExec->GetAtmosphere();
|
|
|
|
FCS = FDMExec->GetFCS();
|
|
|
|
Propulsion = FDMExec->GetPropulsion();
|
|
|
|
Aircraft = FDMExec->GetAircraft();
|
|
|
|
Translation = FDMExec->GetTranslation();
|
|
|
|
Rotation = FDMExec->GetRotation();
|
|
|
|
Position = FDMExec->GetPosition();
|
|
|
|
Auxiliary = FDMExec->GetAuxiliary();
|
|
|
|
Output = FDMExec->GetOutput();
|
|
|
|
|
|
|
|
Mixture = 1.0; // FIXME: get actual value
|
|
|
|
|
|
|
|
Thrust = PctPower = 0.0;
|
|
|
|
Starved = Flameout = false;
|
|
|
|
Running = false;
|
|
|
|
Cranking = Starter = false;
|
|
|
|
|
2001-12-13 04:48:34 +00:00
|
|
|
Debug(0);
|
2001-11-09 04:38:53 +00:00
|
|
|
TrimMode = false;
|
|
|
|
}
|
|
|
|
|
|
|
|
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
|
|
|
|
|
|
|
|
FGEngine::~FGEngine()
|
|
|
|
{
|
2001-12-13 04:48:34 +00:00
|
|
|
Debug(1);
|
2001-11-09 04:38:53 +00:00
|
|
|
}
|
|
|
|
|
|
|
|
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
|
|
|
|
// This base class function should be called from within the
|
|
|
|
// derived class' Calculate() function before any other calculations are done.
|
|
|
|
// This base class method removes fuel from the fuel tanks as appropriate,
|
|
|
|
// and sets the starved flag if necessary.
|
|
|
|
|
2001-11-30 17:49:37 +00:00
|
|
|
void FGEngine::ConsumeFuel(void)
|
|
|
|
{
|
2001-11-20 22:34:24 +00:00
|
|
|
double Fshortage, Oshortage;
|
2001-11-09 04:38:53 +00:00
|
|
|
FGTank* Tank;
|
|
|
|
|
|
|
|
if (TrimMode) return;
|
|
|
|
Fshortage = Oshortage = 0.0;
|
|
|
|
for (unsigned int i=0; i<SourceTanks.size(); i++) {
|
|
|
|
Tank = Propulsion->GetTank(i);
|
|
|
|
if (Tank->GetType() == FGTank::ttFUEL) {
|
|
|
|
Fshortage += Tank->Reduce(CalcFuelNeed()/Propulsion->GetnumSelectedFuelTanks());
|
|
|
|
} else {
|
|
|
|
Oshortage += Tank->Reduce(CalcOxidizerNeed()/Propulsion->GetnumSelectedOxiTanks());
|
|
|
|
}
|
|
|
|
}
|
|
|
|
|
|
|
|
if (Fshortage < 0.00 || Oshortage < 0.00) Starved = true;
|
|
|
|
else Starved = false;
|
|
|
|
}
|
|
|
|
|
|
|
|
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
|
|
|
|
|
2001-11-20 22:34:24 +00:00
|
|
|
double FGEngine::CalcFuelNeed(void) {
|
2001-11-09 04:38:53 +00:00
|
|
|
FuelNeed = SLFuelFlowMax*PctPower*State->Getdt()*Propulsion->GetRate();
|
|
|
|
return FuelNeed;
|
|
|
|
}
|
|
|
|
|
|
|
|
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
|
|
|
|
|
2001-11-20 22:34:24 +00:00
|
|
|
double FGEngine::CalcOxidizerNeed(void) {
|
2001-11-09 04:38:53 +00:00
|
|
|
OxidizerNeed = SLOxiFlowMax*PctPower*State->Getdt()*Propulsion->GetRate();
|
|
|
|
return OxidizerNeed;
|
|
|
|
}
|
|
|
|
|
|
|
|
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
|
|
|
|
|
2001-11-20 22:34:24 +00:00
|
|
|
void FGEngine::SetPlacement(double x, double y, double z, double pitch, double yaw) {
|
2001-11-09 04:38:53 +00:00
|
|
|
X = x;
|
|
|
|
Y = y;
|
|
|
|
Z = z;
|
|
|
|
EnginePitch = pitch;
|
|
|
|
EngineYaw = yaw;
|
|
|
|
}
|
|
|
|
|
|
|
|
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
|
|
|
|
|
|
|
|
void FGEngine::AddFeedTank(int tkID)
|
|
|
|
{
|
|
|
|
SourceTanks.push_back(tkID);
|
|
|
|
}
|
|
|
|
|
|
|
|
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
|
2001-12-13 04:48:34 +00:00
|
|
|
// The bitmasked value choices are as follows:
|
|
|
|
// unset: In this case (the default) JSBSim would only print
|
|
|
|
// out the normally expected messages, essentially echoing
|
|
|
|
// the config files as they are read. If the environment
|
|
|
|
// variable is not set, debug_lvl is set to 1 internally
|
|
|
|
// 0: This requests JSBSim not to output any messages
|
|
|
|
// whatsoever.
|
|
|
|
// 1: This value explicity requests the normal JSBSim
|
|
|
|
// startup messages
|
|
|
|
// 2: This value asks for a message to be printed out when
|
|
|
|
// a class is instantiated
|
|
|
|
// 4: When this value is set, a message is displayed when a
|
|
|
|
// FGModel object executes its Run() method
|
|
|
|
// 8: When this value is set, various runtime state variables
|
|
|
|
// are printed out periodically
|
|
|
|
// 16: When set various parameters are sanity checked and
|
|
|
|
// a message is printed out when they go out of bounds
|
|
|
|
|
|
|
|
void FGEngine::Debug(int from)
|
2001-11-09 04:38:53 +00:00
|
|
|
{
|
2001-12-13 04:48:34 +00:00
|
|
|
if (debug_lvl <= 0) return;
|
|
|
|
|
|
|
|
if (debug_lvl & 1) { // Standard console startup message output
|
|
|
|
if (from == 0) { // Constructor
|
2001-11-09 04:38:53 +00:00
|
|
|
|
2001-12-13 04:48:34 +00:00
|
|
|
}
|
|
|
|
}
|
|
|
|
if (debug_lvl & 2 ) { // Instantiation/Destruction notification
|
|
|
|
if (from == 0) cout << "Instantiated: FGEngine" << endl;
|
|
|
|
if (from == 1) cout << "Destroyed: FGEngine" << endl;
|
|
|
|
}
|
|
|
|
if (debug_lvl & 4 ) { // Run() method entry print for FGModel-derived objects
|
|
|
|
}
|
|
|
|
if (debug_lvl & 8 ) { // Runtime state variables
|
|
|
|
}
|
|
|
|
if (debug_lvl & 16) { // Sanity checking
|
|
|
|
}
|
2001-12-24 13:54:55 +00:00
|
|
|
if (debug_lvl & 64) {
|
|
|
|
if (from == 0) { // Constructor
|
|
|
|
cout << IdSrc << endl;
|
|
|
|
cout << IdHdr << endl;
|
|
|
|
}
|
|
|
|
}
|
2001-12-13 04:48:34 +00:00
|
|
|
}
|
2001-12-24 13:54:55 +00:00
|
|
|
|