2000-11-03 23:02:47 +00:00
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/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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1999-02-05 21:26:01 +00:00
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Module: FGFDMExec.cpp
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Author: Jon S. Berndt
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Date started: 11/17/98
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Purpose: Schedules and runs the model routines.
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------------- Copyright (C) 1999 Jon S. Berndt (jsb@hal-pc.org) -------------
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This program is free software; you can redistribute it and/or modify it under
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the terms of the GNU General Public License as published by the Free Software
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Foundation; either version 2 of the License, or (at your option) any later
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version.
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This program is distributed in the hope that it will be useful, but WITHOUT
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ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS
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FOR A PARTICULAR PURPOSE. See the GNU General Public License for more
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details.
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You should have received a copy of the GNU General Public License along with
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this program; if not, write to the Free Software Foundation, Inc., 59 Temple
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Place - Suite 330, Boston, MA 02111-1307, USA.
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Further information about the GNU General Public License can also be found on
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the world wide web at http://www.gnu.org.
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FUNCTIONAL DESCRIPTION
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--------------------------------------------------------------------------------
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This class wraps up the simulation scheduling routines.
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HISTORY
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--------------------------------------------------------------------------------
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11/17/98 JSB Created
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2001-03-30 01:04:50 +00:00
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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COMMENTS, REFERENCES, and NOTES
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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2000-11-03 23:02:47 +00:00
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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1999-02-05 21:26:01 +00:00
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INCLUDES
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2000-11-03 23:02:47 +00:00
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
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1999-02-05 21:26:01 +00:00
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1999-02-26 22:09:10 +00:00
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#ifdef FGFS
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2000-02-15 03:30:01 +00:00
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# include <simgear/compiler.h>
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2001-06-05 20:58:48 +00:00
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# include STL_IOSTREAM
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# include STL_ITERATOR
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1999-02-26 22:09:10 +00:00
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#else
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2001-10-05 20:19:59 +00:00
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# if defined(sgi) && !defined(__GNUC__)
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# include <iostream.h>
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# else
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# include <iostream>
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# endif
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2001-03-30 01:04:50 +00:00
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# include <iterator>
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1999-02-26 22:09:10 +00:00
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#endif
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1999-02-05 21:26:01 +00:00
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1999-02-11 21:05:34 +00:00
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#include "FGFDMExec.h"
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#include "FGState.h"
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#include "FGAtmosphere.h"
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#include "FGFCS.h"
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2001-03-30 01:04:50 +00:00
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#include "FGPropulsion.h"
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2001-06-05 20:58:48 +00:00
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#include "FGMassBalance.h"
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2001-10-05 20:19:59 +00:00
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#include "FGGroundReactions.h"
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2001-06-05 20:58:48 +00:00
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#include "FGAerodynamics.h"
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#include "FGInertial.h"
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1999-02-11 21:05:34 +00:00
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#include "FGAircraft.h"
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#include "FGTranslation.h"
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#include "FGRotation.h"
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#include "FGPosition.h"
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#include "FGAuxiliary.h"
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#include "FGOutput.h"
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2001-03-30 01:04:50 +00:00
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#include "FGConfigFile.h"
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2001-12-14 03:35:41 +00:00
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#include "FGInitialCondition.h"
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2002-03-20 12:45:02 +00:00
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#include "FGPropertyManager.h"
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1999-02-11 21:05:34 +00:00
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2001-03-30 01:04:50 +00:00
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static const char *IdSrc = "$Id$";
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2001-06-05 20:58:48 +00:00
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static const char *IdHdr = ID_FDMEXEC;
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2000-10-14 02:10:10 +00:00
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2000-11-03 23:02:47 +00:00
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/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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2001-03-30 01:04:50 +00:00
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GLOBAL DECLARATIONS
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2000-11-03 23:02:47 +00:00
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
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1999-02-05 21:26:01 +00:00
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2001-11-12 16:06:29 +00:00
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unsigned int FGFDMExec::FDMctr = 0;
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2002-03-23 00:29:21 +00:00
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FGPropertyManager* FGFDMExec::master=0;
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2001-11-12 16:06:29 +00:00
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2001-03-30 01:04:50 +00:00
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/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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CLASS IMPLEMENTATION
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
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1999-02-05 21:26:01 +00:00
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// Constructor
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2002-03-20 12:45:02 +00:00
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FGFDMExec::FGFDMExec(FGPropertyManager* root)
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1999-02-05 21:26:01 +00:00
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{
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2002-03-20 12:45:02 +00:00
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2001-10-05 20:19:59 +00:00
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Frame = 0;
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FirstModel = 0;
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Error = 0;
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State = 0;
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Atmosphere = 0;
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FCS = 0;
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Propulsion = 0;
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MassBalance = 0;
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Aerodynamics = 0;
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Inertial = 0;
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GroundReactions = 0;
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Aircraft = 0;
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Translation = 0;
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Rotation = 0;
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Position = 0;
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Auxiliary = 0;
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Output = 0;
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1999-02-11 21:05:34 +00:00
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2000-10-10 17:44:35 +00:00
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terminate = false;
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frozen = false;
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2000-10-12 01:06:31 +00:00
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modelLoaded = false;
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2002-03-23 00:29:21 +00:00
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IsSlave = false;
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2001-03-30 01:04:50 +00:00
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2001-11-12 16:06:29 +00:00
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IdFDM = FDMctr;
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FDMctr++;
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2001-03-30 01:04:50 +00:00
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try {
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char* num = getenv("JSBSIM_DEBUG");
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if (!num) debug_lvl = 1;
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else debug_lvl = atoi(num); // set debug level
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} catch (...) { // if error set to 1
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debug_lvl = 1;
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}
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2002-03-23 00:29:21 +00:00
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if (root == 0) master= new FGPropertyManager;
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else master = root;
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2001-03-30 01:04:50 +00:00
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2002-03-20 12:45:02 +00:00
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instance = master->GetNode("/fdm/jsbsim",IdFDM,true);
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instance->SetDouble("zero",0);
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Debug(0);
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// this is here to catch errors in binding member functions
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// to the property tree.
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try {
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Allocate();
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} catch ( string msg ) {
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cout << "Caught error: " << msg << endl;
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exit(1);
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}
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2000-10-10 17:44:35 +00:00
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}
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2001-03-30 01:04:50 +00:00
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//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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1999-02-11 21:05:34 +00:00
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2001-12-13 04:48:34 +00:00
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FGFDMExec::~FGFDMExec()
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{
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2002-03-20 12:45:02 +00:00
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try {
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DeAllocate();
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} catch ( string msg ) {
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cout << "Caught error: " << msg << endl;
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}
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2001-12-13 04:48:34 +00:00
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2002-03-23 00:29:21 +00:00
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for (int i=1; i<SlaveFDMList.size(); i++) delete SlaveFDMList[i]->exec;
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SlaveFDMList.clear();
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2001-12-13 04:48:34 +00:00
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Debug(1);
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2000-10-10 17:44:35 +00:00
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}
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2001-03-30 01:04:50 +00:00
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//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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2001-12-13 04:48:34 +00:00
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bool FGFDMExec::Allocate(void)
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{
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2000-10-10 17:44:35 +00:00
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bool result=true;
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2001-03-30 01:04:50 +00:00
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2001-10-05 20:19:59 +00:00
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Atmosphere = new FGAtmosphere(this);
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FCS = new FGFCS(this);
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Propulsion = new FGPropulsion(this);
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MassBalance = new FGMassBalance(this);
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Aerodynamics = new FGAerodynamics (this);
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Inertial = new FGInertial(this);
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GroundReactions = new FGGroundReactions(this);
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Aircraft = new FGAircraft(this);
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Translation = new FGTranslation(this);
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Rotation = new FGRotation(this);
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Position = new FGPosition(this);
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Auxiliary = new FGAuxiliary(this);
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Output = new FGOutput(this);
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2001-06-05 20:58:48 +00:00
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State = new FGState(this); // This must be done here, as the FGState
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// class needs valid pointers to the above
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2001-10-05 20:19:59 +00:00
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// model classes
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1999-02-11 21:05:34 +00:00
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// Initialize models so they can communicate with each other
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2001-03-30 01:04:50 +00:00
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if (!Atmosphere->InitModel()) {
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cerr << fgred << "Atmosphere model init failed" << fgdef << endl;
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Error+=1;}
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if (!FCS->InitModel()) {
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cerr << fgred << "FCS model init failed" << fgdef << endl;
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Error+=2;}
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if (!Propulsion->InitModel()) {
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cerr << fgred << "FGPropulsion model init failed" << fgdef << endl;
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Error+=4;}
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2001-06-05 20:58:48 +00:00
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if (!MassBalance->InitModel()) {
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cerr << fgred << "FGMassBalance model init failed" << fgdef << endl;
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Error+=8;}
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if (!Aerodynamics->InitModel()) {
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cerr << fgred << "FGAerodynamics model init failed" << fgdef << endl;
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Error+=16;}
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if (!Inertial->InitModel()) {
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cerr << fgred << "FGInertial model init failed" << fgdef << endl;
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Error+=32;}
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2001-10-05 20:19:59 +00:00
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if (!GroundReactions->InitModel()) {
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cerr << fgred << "Ground Reactions model init failed" << fgdef << endl;
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Error+=64;}
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2001-03-30 01:04:50 +00:00
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if (!Aircraft->InitModel()) {
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cerr << fgred << "Aircraft model init failed" << fgdef << endl;
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2001-10-05 20:19:59 +00:00
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Error+=128;}
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2002-04-16 13:15:29 +00:00
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if (!Translation->InitModel()) {
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2001-03-30 01:04:50 +00:00
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cerr << fgred << "Translation model init failed" << fgdef << endl;
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2001-10-05 20:19:59 +00:00
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Error+=256;}
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2001-03-30 01:04:50 +00:00
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if (!Rotation->InitModel()) {
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cerr << fgred << "Rotation model init failed" << fgdef << endl;
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2001-10-05 20:19:59 +00:00
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Error+=512;}
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2001-03-30 01:04:50 +00:00
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if (!Position->InitModel()) {
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cerr << fgred << "Position model init failed" << fgdef << endl;
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2001-10-05 20:19:59 +00:00
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Error+=1024;}
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2001-03-30 01:04:50 +00:00
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if (!Auxiliary->InitModel()) {
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cerr << fgred << "Auxiliary model init failed" << fgdef << endl;
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2001-10-05 20:19:59 +00:00
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Error+=2058;}
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2001-03-30 01:04:50 +00:00
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if (!Output->InitModel()) {
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cerr << fgred << "Output model init failed" << fgdef << endl;
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2001-10-05 20:19:59 +00:00
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Error+=4096;}
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2001-03-30 01:04:50 +00:00
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if (Error > 0) result = false;
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1999-08-17 21:18:11 +00:00
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// Schedule a model. The second arg (the integer) is the pass number. For
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// instance, the atmosphere model gets executed every fifth pass it is called
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// by the executive. Everything else here gets executed each pass.
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1999-02-05 21:26:01 +00:00
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2001-10-05 20:19:59 +00:00
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Schedule(Atmosphere, 1);
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Schedule(FCS, 1);
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Schedule(Propulsion, 1);
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Schedule(MassBalance, 1);
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Schedule(Aerodynamics, 1);
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Schedule(Inertial, 1);
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Schedule(GroundReactions, 1);
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Schedule(Aircraft, 1);
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Schedule(Rotation, 1);
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Schedule(Translation, 1);
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Schedule(Position, 1);
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Schedule(Auxiliary, 1);
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Schedule(Output, 1);
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2001-03-30 01:04:50 +00:00
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2000-10-12 01:06:31 +00:00
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modelLoaded = false;
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1999-02-05 21:26:01 +00:00
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2001-03-30 01:04:50 +00:00
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return result;
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1999-02-05 21:26:01 +00:00
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}
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2001-03-30 01:04:50 +00:00
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//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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2000-10-10 17:44:35 +00:00
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bool FGFDMExec::DeAllocate(void) {
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2001-03-30 01:04:50 +00:00
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2001-10-05 20:19:59 +00:00
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if ( Atmosphere != 0 ) delete Atmosphere;
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if ( FCS != 0 ) delete FCS;
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if ( Propulsion != 0) delete Propulsion;
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if ( MassBalance != 0) delete MassBalance;
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if ( Aerodynamics != 0) delete Aerodynamics;
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if ( Inertial != 0) delete Inertial;
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if ( GroundReactions != 0) delete GroundReactions;
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if ( Aircraft != 0 ) delete Aircraft;
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if ( Translation != 0 ) delete Translation;
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if ( Rotation != 0 ) delete Rotation;
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if ( Position != 0 ) delete Position;
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if ( Auxiliary != 0 ) delete Auxiliary;
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if ( Output != 0 ) delete Output;
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if ( State != 0 ) delete State;
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2000-10-12 01:06:31 +00:00
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FirstModel = 0L;
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Error = 0;
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2001-10-05 20:19:59 +00:00
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State = 0;
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Atmosphere = 0;
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FCS = 0;
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Propulsion = 0;
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MassBalance = 0;
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Aerodynamics = 0;
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Inertial = 0;
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GroundReactions = 0;
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Aircraft = 0;
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Translation = 0;
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Rotation = 0;
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Position = 0;
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Auxiliary = 0;
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Output = 0;
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2000-10-12 01:06:31 +00:00
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modelLoaded = false;
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2001-03-30 01:04:50 +00:00
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return modelLoaded;
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1999-02-05 21:26:01 +00:00
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}
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2001-03-30 01:04:50 +00:00
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//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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1999-02-05 21:26:01 +00:00
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int FGFDMExec::Schedule(FGModel* model, int rate)
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{
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FGModel* model_iterator;
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model_iterator = FirstModel;
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if (model_iterator == 0L) { // this is the first model
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FirstModel = model;
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FirstModel->NextModel = 0L;
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FirstModel->SetRate(rate);
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} else { // subsequent model
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while (model_iterator->NextModel != 0L) {
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model_iterator = model_iterator->NextModel;
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}
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model_iterator->NextModel = model;
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|
|
model_iterator->NextModel->SetRate(rate);
|
|
|
|
|
|
|
|
}
|
2001-11-20 22:34:24 +00:00
|
|
|
|
1999-02-05 21:26:01 +00:00
|
|
|
return 0;
|
|
|
|
}
|
|
|
|
|
2001-03-30 01:04:50 +00:00
|
|
|
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
|
1999-02-05 21:26:01 +00:00
|
|
|
|
|
|
|
bool FGFDMExec::Run(void)
|
|
|
|
{
|
|
|
|
FGModel* model_iterator;
|
|
|
|
|
1999-02-11 21:05:34 +00:00
|
|
|
if (frozen) return true;
|
|
|
|
|
1999-02-05 21:26:01 +00:00
|
|
|
model_iterator = FirstModel;
|
|
|
|
if (model_iterator == 0L) return false;
|
|
|
|
|
2001-12-13 04:48:34 +00:00
|
|
|
Debug(2);
|
2001-03-30 01:04:50 +00:00
|
|
|
|
2002-03-23 00:29:21 +00:00
|
|
|
for (int i=0; i<SlaveFDMList.size(); i++) {
|
|
|
|
// TransferState(i);
|
|
|
|
// Run(i)
|
|
|
|
}
|
|
|
|
|
2001-03-30 01:04:50 +00:00
|
|
|
while (!model_iterator->Run()) {
|
1999-02-05 21:26:01 +00:00
|
|
|
model_iterator = model_iterator->NextModel;
|
|
|
|
if (model_iterator == 0L) break;
|
|
|
|
}
|
|
|
|
|
2001-11-24 22:13:04 +00:00
|
|
|
frame = Frame++;
|
1999-02-11 21:05:34 +00:00
|
|
|
State->IncrTime();
|
|
|
|
|
1999-02-05 21:26:01 +00:00
|
|
|
return true;
|
|
|
|
}
|
|
|
|
|
2001-03-30 01:04:50 +00:00
|
|
|
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
|
2000-05-02 18:25:30 +00:00
|
|
|
|
1999-08-17 21:18:11 +00:00
|
|
|
bool FGFDMExec::RunIC(FGInitialCondition *fgic)
|
|
|
|
{
|
2000-10-02 23:07:30 +00:00
|
|
|
State->Suspend();
|
1999-08-17 21:18:11 +00:00
|
|
|
State->Initialize(fgic);
|
|
|
|
Run();
|
2000-10-02 23:07:30 +00:00
|
|
|
State->Resume();
|
1999-08-17 21:18:11 +00:00
|
|
|
return true;
|
|
|
|
}
|
2001-03-30 01:04:50 +00:00
|
|
|
|
|
|
|
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
|
1999-08-17 21:18:11 +00:00
|
|
|
|
2002-03-23 00:29:21 +00:00
|
|
|
void FGFDMExec::TransferState(int idxFDM)
|
|
|
|
{
|
|
|
|
SlaveFDMList[idxFDM]->exec->GetRotation()->SetEuler(Rotation->GetEuler());
|
|
|
|
SlaveFDMList[idxFDM]->exec->GetRotation()->SetAeroPQR(Rotation->GetAeroPQR());
|
|
|
|
SlaveFDMList[idxFDM]->exec->GetTranslation()->SetAeroUVW(Translation->GetAeroUVW());
|
|
|
|
SlaveFDMList[idxFDM]->exec->GetRotation()->SetEuler(Rotation->GetEuler());
|
|
|
|
}
|
|
|
|
|
|
|
|
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
|
|
|
|
|
|
|
|
vector <string> FGFDMExec::EnumerateFDMs(void)
|
|
|
|
{
|
|
|
|
vector <string> FDMList;
|
|
|
|
|
|
|
|
FDMList.push_back(Aircraft->GetAircraftName());
|
|
|
|
|
|
|
|
for (int i=1; i<SlaveFDMList.size(); i++) {
|
|
|
|
FDMList.push_back(SlaveFDMList[i]->exec->GetAircraft()->GetAircraftName());
|
|
|
|
}
|
|
|
|
|
|
|
|
return FDMList;
|
|
|
|
}
|
|
|
|
|
|
|
|
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
|
|
|
|
|
2000-10-02 23:07:30 +00:00
|
|
|
bool FGFDMExec::LoadModel(string APath, string EPath, string model)
|
|
|
|
{
|
2001-12-24 13:54:55 +00:00
|
|
|
bool result = true;
|
|
|
|
string token;
|
2001-07-10 15:56:38 +00:00
|
|
|
string aircraftCfgFileName;
|
|
|
|
|
|
|
|
AircraftPath = APath;
|
|
|
|
EnginePath = EPath;
|
|
|
|
|
|
|
|
# ifndef macintosh
|
|
|
|
aircraftCfgFileName = AircraftPath + "/" + model + "/" + model + ".xml";
|
|
|
|
# else
|
|
|
|
aircraftCfgFileName = AircraftPath + ";" + model + ";" + model + ".xml";
|
|
|
|
# endif
|
|
|
|
|
|
|
|
FGConfigFile AC_cfg(aircraftCfgFileName);
|
|
|
|
if (!AC_cfg.IsOpen()) return false;
|
|
|
|
|
2001-03-30 01:04:50 +00:00
|
|
|
if (modelLoaded) {
|
|
|
|
DeAllocate();
|
|
|
|
Allocate();
|
|
|
|
}
|
2001-06-05 20:58:48 +00:00
|
|
|
|
2001-12-24 13:54:55 +00:00
|
|
|
if (!ReadPrologue(&AC_cfg)) return false;
|
|
|
|
|
|
|
|
while ((AC_cfg.GetNextConfigLine() != string("EOF")) &&
|
|
|
|
(token = AC_cfg.GetValue()) != string("/FDM_CONFIG")) {
|
|
|
|
if (token == "METRICS") {
|
|
|
|
if (debug_lvl > 0) cout << fgcyan << "\n Reading Metrics" << fgdef << endl;
|
|
|
|
if (!ReadMetrics(&AC_cfg)) result = false;
|
2002-03-23 00:29:21 +00:00
|
|
|
} else if (token == "SLAVE") {
|
|
|
|
if (debug_lvl > 0) cout << fgcyan << "\n Reading Slave flight vehicle: " << fgdef
|
|
|
|
<< AC_cfg.GetValue("NAME") << endl;
|
|
|
|
if (!ReadSlave(&AC_cfg)) result = false;
|
2001-12-24 13:54:55 +00:00
|
|
|
} else if (token == "AERODYNAMICS") {
|
|
|
|
if (debug_lvl > 0) cout << fgcyan << "\n Reading Aerodynamics" << fgdef << endl;
|
|
|
|
if (!ReadAerodynamics(&AC_cfg)) result = false;
|
|
|
|
} else if (token == "UNDERCARRIAGE") {
|
|
|
|
if (debug_lvl > 0) cout << fgcyan << "\n Reading Landing Gear" << fgdef << endl;
|
|
|
|
if (!ReadUndercarriage(&AC_cfg)) result = false;
|
|
|
|
} else if (token == "PROPULSION") {
|
|
|
|
if (debug_lvl > 0) cout << fgcyan << "\n Reading Propulsion" << fgdef << endl;
|
|
|
|
if (!ReadPropulsion(&AC_cfg)) result = false;
|
|
|
|
} else if (token == "FLIGHT_CONTROL") {
|
|
|
|
if (debug_lvl > 0) cout << fgcyan << "\n Reading Flight Control" << fgdef << endl;
|
|
|
|
if (!ReadFlightControls(&AC_cfg)) result = false;
|
|
|
|
} else if (token == "OUTPUT") {
|
|
|
|
if (debug_lvl > 0) cout << fgcyan << "\n Reading Output directives" << fgdef << endl;
|
|
|
|
if (!ReadOutput(&AC_cfg)) result = false;
|
|
|
|
}
|
|
|
|
}
|
2000-11-03 23:02:47 +00:00
|
|
|
|
|
|
|
if (result) {
|
|
|
|
modelLoaded = true;
|
2001-12-13 04:48:34 +00:00
|
|
|
Debug(3);
|
2000-10-12 01:06:31 +00:00
|
|
|
} else {
|
2001-03-30 01:04:50 +00:00
|
|
|
cerr << fgred
|
2001-12-01 04:03:57 +00:00
|
|
|
<< " FGFDMExec: Failed to load aircraft and/or engine model"
|
2001-03-30 01:04:50 +00:00
|
|
|
<< fgdef << endl;
|
2000-11-03 23:02:47 +00:00
|
|
|
}
|
|
|
|
|
2000-10-12 01:06:31 +00:00
|
|
|
return result;
|
2000-10-02 23:07:30 +00:00
|
|
|
}
|
|
|
|
|
2001-03-30 01:04:50 +00:00
|
|
|
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
|
|
|
|
|
2001-12-24 13:54:55 +00:00
|
|
|
bool FGFDMExec::ReadPrologue(FGConfigFile* AC_cfg)
|
2001-03-30 01:04:50 +00:00
|
|
|
{
|
2001-12-24 13:54:55 +00:00
|
|
|
string token = AC_cfg->GetValue();
|
|
|
|
string scratch;
|
|
|
|
string AircraftName;
|
2002-03-23 00:29:21 +00:00
|
|
|
|
2001-12-24 13:54:55 +00:00
|
|
|
AircraftName = AC_cfg->GetValue("NAME");
|
|
|
|
Aircraft->SetAircraftName(AircraftName);
|
|
|
|
|
|
|
|
if (debug_lvl > 0) cout << underon << "Reading Aircraft Configuration File"
|
|
|
|
<< underoff << ": " << highint << AircraftName << normint << endl;
|
|
|
|
scratch = AC_cfg->GetValue("VERSION").c_str();
|
|
|
|
|
|
|
|
CFGVersion = AC_cfg->GetValue("VERSION");
|
|
|
|
|
|
|
|
if (debug_lvl > 0)
|
|
|
|
cout << " Version: " << highint << CFGVersion
|
2002-03-23 00:29:21 +00:00
|
|
|
<< normint << endl;
|
2001-12-24 13:54:55 +00:00
|
|
|
if (CFGVersion != needed_cfg_version) {
|
|
|
|
cerr << endl << fgred << "YOU HAVE AN INCOMPATIBLE CFG FILE FOR THIS AIRCRAFT."
|
|
|
|
" RESULTS WILL BE UNPREDICTABLE !!" << endl;
|
|
|
|
cerr << "Current version needed is: " << needed_cfg_version << endl;
|
|
|
|
cerr << " You have version: " << CFGVersion << endl << fgdef << endl;
|
|
|
|
return false;
|
2001-03-30 01:04:50 +00:00
|
|
|
}
|
2002-03-23 00:29:21 +00:00
|
|
|
|
|
|
|
return true;
|
|
|
|
}
|
|
|
|
|
|
|
|
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
|
|
|
|
|
|
|
|
bool FGFDMExec::ReadSlave(FGConfigFile* AC_cfg)
|
|
|
|
{
|
|
|
|
// Add a new slaveData object to the slave FDM list
|
|
|
|
// Populate that slaveData element with a new FDMExec object
|
|
|
|
// Set the IsSlave flag for that FDMExec object
|
|
|
|
// Get the aircraft name
|
|
|
|
// set debug level to print out no additional data for slave objects
|
|
|
|
// Load the model given the aircraft name
|
|
|
|
// reset debug level to prior setting
|
|
|
|
|
|
|
|
int saved_debug_lvl = debug_lvl;
|
|
|
|
|
|
|
|
SlaveFDMList.push_back(new slaveData);
|
|
|
|
SlaveFDMList.back()->exec = new FGFDMExec();
|
|
|
|
SlaveFDMList.back()->exec->SetSlave();
|
|
|
|
|
|
|
|
string AircraftName = AC_cfg->GetValue("FILE");
|
|
|
|
|
|
|
|
debug_lvl = 0;
|
|
|
|
SlaveFDMList.back()->exec->LoadModel("aircraft", "engine", AircraftName);
|
|
|
|
debug_lvl = saved_debug_lvl;
|
|
|
|
|
2001-12-24 13:54:55 +00:00
|
|
|
return true;
|
|
|
|
}
|
2001-03-30 01:04:50 +00:00
|
|
|
|
2001-12-24 13:54:55 +00:00
|
|
|
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
|
|
|
|
|
|
|
|
bool FGFDMExec::ReadPropulsion(FGConfigFile* AC_cfg)
|
|
|
|
{
|
|
|
|
if (!Propulsion->Load(AC_cfg)) {
|
|
|
|
cerr << " Propulsion not successfully loaded" << endl;
|
|
|
|
return false;
|
2001-03-30 01:04:50 +00:00
|
|
|
}
|
2001-12-24 13:54:55 +00:00
|
|
|
return true;
|
|
|
|
}
|
2001-03-30 01:04:50 +00:00
|
|
|
|
2001-12-24 13:54:55 +00:00
|
|
|
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
|
2001-03-30 01:04:50 +00:00
|
|
|
|
2001-12-24 13:54:55 +00:00
|
|
|
bool FGFDMExec::ReadFlightControls(FGConfigFile* AC_cfg)
|
|
|
|
{
|
|
|
|
if (!FCS->Load(AC_cfg)) {
|
|
|
|
cerr << " Flight Controls not successfully loaded" << endl;
|
|
|
|
return false;
|
2001-03-30 01:04:50 +00:00
|
|
|
}
|
2001-12-24 13:54:55 +00:00
|
|
|
return true;
|
|
|
|
}
|
|
|
|
|
|
|
|
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
|
2001-03-30 01:04:50 +00:00
|
|
|
|
2001-12-24 13:54:55 +00:00
|
|
|
bool FGFDMExec::ReadAerodynamics(FGConfigFile* AC_cfg)
|
|
|
|
{
|
|
|
|
if (!Aerodynamics->Load(AC_cfg)) {
|
|
|
|
cerr << " Aerodynamics not successfully loaded" << endl;
|
|
|
|
return false;
|
2001-12-14 03:35:41 +00:00
|
|
|
}
|
2001-12-24 13:54:55 +00:00
|
|
|
return true;
|
|
|
|
}
|
2001-12-14 03:35:41 +00:00
|
|
|
|
2001-12-24 13:54:55 +00:00
|
|
|
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
|
|
|
|
|
|
|
|
bool FGFDMExec::ReadUndercarriage(FGConfigFile* AC_cfg)
|
|
|
|
{
|
|
|
|
if (!GroundReactions->Load(AC_cfg)) {
|
|
|
|
cerr << " Ground Reactions not successfully loaded" << endl;
|
|
|
|
return false;
|
|
|
|
}
|
2001-03-30 01:04:50 +00:00
|
|
|
return true;
|
|
|
|
}
|
|
|
|
|
|
|
|
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
|
2000-10-02 23:07:30 +00:00
|
|
|
|
2001-12-24 13:54:55 +00:00
|
|
|
bool FGFDMExec::ReadMetrics(FGConfigFile* AC_cfg)
|
2000-10-02 23:07:30 +00:00
|
|
|
{
|
2001-12-24 13:54:55 +00:00
|
|
|
if (!Aircraft->Load(AC_cfg)) {
|
|
|
|
cerr << " Aircraft metrics not successfully loaded" << endl;
|
|
|
|
return false;
|
|
|
|
}
|
|
|
|
return true;
|
|
|
|
}
|
2001-03-30 01:04:50 +00:00
|
|
|
|
2001-12-24 13:54:55 +00:00
|
|
|
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
|
|
|
|
|
|
|
|
bool FGFDMExec::ReadOutput(FGConfigFile* AC_cfg)
|
|
|
|
{
|
|
|
|
if (!Output->Load(AC_cfg)) {
|
|
|
|
cerr << " Output not successfully loaded" << endl;
|
|
|
|
return false;
|
2001-03-30 01:04:50 +00:00
|
|
|
}
|
2001-12-24 13:54:55 +00:00
|
|
|
return true;
|
2000-10-02 23:07:30 +00:00
|
|
|
}
|
2001-03-30 01:04:50 +00:00
|
|
|
|
2002-03-20 12:45:02 +00:00
|
|
|
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
|
|
|
|
|
|
|
|
FGPropertyManager* FGFDMExec::GetPropertyManager(void) {
|
|
|
|
return instance;
|
|
|
|
}
|
|
|
|
|
2001-03-30 01:04:50 +00:00
|
|
|
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
|
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 FGFDMExec::Debug(int from)
|
2001-03-30 01:04:50 +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
|
|
|
|
cout << "\n\n " << highint << underon << "JSBSim Flight Dynamics Model v"
|
|
|
|
<< JSBSim_version << underoff << normint << endl;
|
|
|
|
cout << halfint << " [cfg file spec v" << needed_cfg_version << "]\n\n";
|
|
|
|
cout << normint << "JSBSim startup beginning ...\n\n";
|
|
|
|
} else if (from == 3) {
|
|
|
|
cout << "\n\nJSBSim startup complete\n\n";
|
|
|
|
}
|
|
|
|
}
|
|
|
|
if (debug_lvl & 2 ) { // Instantiation/Destruction notification
|
|
|
|
if (from == 0) cout << "Instantiated: FGFDMExec" << endl;
|
|
|
|
if (from == 1) cout << "Destroyed: FGFDMExec" << endl;
|
|
|
|
}
|
|
|
|
if (debug_lvl & 4 ) { // Run() method entry print for FGModel-derived objects
|
|
|
|
if (from == 2) {
|
|
|
|
cout << "================== Frame: " << Frame << " Time: "
|
|
|
|
<< State->Getsim_time() << endl;
|
|
|
|
}
|
|
|
|
}
|
|
|
|
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
|
|
|
|