Date started: 12/12/98
Purpose: Encapsulates an aircraft
Called by: FGFDMExec
-
+
------------- Copyright (C) 1999 Jon S. Berndt (jsb@hal-pc.org) -------------
This program is free software; you can redistribute it and/or modify it under
FUNCTIONAL DESCRIPTION
--------------------------------------------------------------------------------
Models the aircraft reactions and forces. This class is instantiated by the
-FGFDMExec class and scheduled as an FDM entry. LoadAircraft() is supplied with a
-name of a valid, registered aircraft, and the data file is parsed.
+FGFDMExec class and scheduled as an FDM entry.
HISTORY
--------------------------------------------------------------------------------
# ifndef __BORLANDC__
# include <simgear/compiler.h>
# endif
-# ifdef FG_HAVE_STD_INCLUDES
+# ifdef SG_HAVE_STD_INCLUDES
# include <cmath>
# else
# include <math.h>
#endif
#include "FGAircraft.h"
+#include "FGMassBalance.h"
+#include "FGInertial.h"
+#include "FGAerodynamics.h"
#include "FGTranslation.h"
#include "FGRotation.h"
#include "FGAtmosphere.h"
FGAircraft::FGAircraft(FGFDMExec* fdmex) : FGModel(fdmex),
vMoments(3),
vForces(3),
- vFs(3),
vXYZrp(3),
- vbaseXYZcg(3),
- vXYZcg(3),
vXYZep(3),
- vEuler(3)
-
+ vEuler(3),
+ vDXYZcg(3),
+ vAeroBodyForces(3)
{
Name = "FGAircraft";
- AxisIdx["DRAG"] = 0;
- AxisIdx["SIDE"] = 1;
- AxisIdx["LIFT"] = 2;
- AxisIdx["ROLL"] = 3;
- AxisIdx["PITCH"] = 4;
- AxisIdx["YAW"] = 5;
-
- Coeff = new CoeffArray[6];
-
GearUp = false;
alphaclmin = alphaclmax = 0;
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-FGAircraft::~FGAircraft() {
- unsigned int i,j;
- for (i=0; i<6; i++) {
- for (j=0; j<Coeff[i].size(); j++) {
- delete Coeff[i][j];
- }
- }
- delete[] Coeff;
-
+FGAircraft::~FGAircraft()
+{
if (debug_lvl & 2) cout << "Destroyed: FGAircraft" << endl;
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-bool FGAircraft::LoadAircraft(string aircraft_path, string engine_path, string fname) {
- string path;
- string filename;
- string aircraftCfgFileName;
+bool FGAircraft::Load(FGConfigFile* AC_cfg)
+{
string token;
- AircraftPath = aircraft_path;
- EnginePath = engine_path;
-
-# ifndef macintosh
- aircraftCfgFileName = AircraftPath + "/" + fname + "/" + fname + ".xml";
-# else
- aircraftCfgFileName = AircraftPath + ";" + fname + ";" + fname + ".xml";
-# endif
+ ReadPrologue(AC_cfg);
- FGConfigFile AC_cfg(aircraftCfgFileName);
- if (!AC_cfg.IsOpen()) return false;
-
- ReadPrologue(&AC_cfg);
-
- while ((AC_cfg.GetNextConfigLine() != string("EOF")) &&
- (token = AC_cfg.GetValue()) != string("/FDM_CONFIG")) {
+ while ((AC_cfg->GetNextConfigLine() != "EOF") &&
+ (token = AC_cfg->GetValue()) != "/FDM_CONFIG") {
if (token == "METRICS") {
- cout << fgcyan << "\n Reading Metrics" << fgdef << endl;
- ReadMetrics(&AC_cfg);
+ if (debug_lvl > 0) cout << fgcyan << "\n Reading Metrics" << fgdef << endl;
+ ReadMetrics(AC_cfg);
} else if (token == "AERODYNAMICS") {
- cout << fgcyan << "\n Reading Aerodynamics" << fgdef << endl;
- ReadAerodynamics(&AC_cfg);
+ if (debug_lvl > 0) cout << fgcyan << "\n Reading Aerodynamics" << fgdef << endl;
+ ReadAerodynamics(AC_cfg);
} else if (token == "UNDERCARRIAGE") {
- cout << fgcyan << "\n Reading Landing Gear" << fgdef << endl;
- ReadUndercarriage(&AC_cfg);
+ if (debug_lvl > 0) cout << fgcyan << "\n Reading Landing Gear" << fgdef << endl;
+ ReadUndercarriage(AC_cfg);
} else if (token == "PROPULSION") {
- cout << fgcyan << "\n Reading Propulsion" << fgdef << endl;
- ReadPropulsion(&AC_cfg);
+ if (debug_lvl > 0) cout << fgcyan << "\n Reading Propulsion" << fgdef << endl;
+ ReadPropulsion(AC_cfg);
} else if (token == "FLIGHT_CONTROL") {
- cout << fgcyan << "\n Reading Flight Control" << fgdef << endl;
- ReadFlightControls(&AC_cfg);
+ if (debug_lvl > 0) cout << fgcyan << "\n Reading Flight Control" << fgdef << endl;
+ ReadFlightControls(AC_cfg);
} else if (token == "OUTPUT") {
- cout << fgcyan << "\n Reading Output directives" << fgdef << endl;
- ReadOutput(&AC_cfg);
+ if (debug_lvl > 0) cout << fgcyan << "\n Reading Output directives" << fgdef << endl;
+ ReadOutput(AC_cfg);
}
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-bool FGAircraft::Run(void) {
+bool FGAircraft::Run(void)
+{
if (!FGModel::Run()) { // if false then execute this Run()
GetState();
- for (int i = 1; i <= 3; i++) vForces(i) = vMoments(i) = 0.0;
+ vForces.InitMatrix();
+ vMoments.InitMatrix();
- MassChange();
FMProp();
FMAero();
- FMGear();
FMMass();
+ FMGear();
- nlf = 0;
- if (fabs(Position->GetGamma()) < 1.57) {
- nlf = vFs(eZ)/(Weight*cos(Position->GetGamma()));
- }
-
+ return false;
} else { // skip Run() execution this time
+ return true;
}
-
-
- return false;
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-void FGAircraft::MassChange() {
- static FGColumnVector vXYZtank(3);
- float Tw;
- float IXXt, IYYt, IZZt, IXZt;
-// unsigned int t;
-// unsigned int axis_ctr;
-/*
- for (axis_ctr=1; axis_ctr<=3; axis_ctr++) vXYZtank(axis_ctr) = 0.0;
-
- // UPDATE TANK CONTENTS
- //
- // For each engine, cycle through the tanks and draw an equal amount of
- // fuel (or oxidizer) from each active tank. The needed amount of fuel is
- // determined by the engine in the FGEngine class. If more fuel is needed
- // than is available in the tank, then that amount is considered a shortage,
- // and will be drawn from the next tank. If the engine cannot be fed what it
- // needs, it will be considered to be starved, and will shut down.
-
- float Oshortage, Fshortage;
-
- for (unsigned int e=0; e<numEngines; e++) {
- Fshortage = Oshortage = 0.0;
- for (t=0; t<numTanks; t++) {
- switch(Engine[e]->GetType()) {
- case FGEngine::etRocket:
-
- switch(Tank[t]->GetType()) {
- case FGTank::ttFUEL:
- if (Tank[t]->GetSelected()) {
- Fshortage = Tank[t]->Reduce((Engine[e]->CalcFuelNeed()/
- numSelectedFuelTanks)*(dt*rate) + Fshortage);
- }
- break;
- case FGTank::ttOXIDIZER:
- if (Tank[t]->GetSelected()) {
- Oshortage = Tank[t]->Reduce((Engine[e]->CalcOxidizerNeed()/
- numSelectedOxiTanks)*(dt*rate) + Oshortage);
- }
- break;
- }
- break;
-
- case FGEngine::etPiston:
- case FGEngine::etTurboJet:
- case FGEngine::etTurboProp:
-
- if (Tank[t]->GetSelected()) {
- Fshortage = Tank[t]->Reduce((Engine[e]->CalcFuelNeed()/
- numSelectedFuelTanks)*(dt*rate) + Fshortage);
- }
- break;
- }
- }
- if ((Fshortage <= 0.0) || (Oshortage <= 0.0)) Engine[e]->SetStarved();
- else Engine[e]->SetStarved(false);
- }
-*/
- Weight = EmptyWeight;
-// for (t=0; t<numTanks; t++)
-// Weight += Tank[t]->GetContents();
-
- Mass = Weight / GRAVITY;
- // Calculate new CG here.
-
- Tw = 0;
-// for (t=0; t<numTanks; t++) {
-// vXYZtank(eX) += Tank[t]->GetX()*Tank[t]->GetContents();
-// vXYZtank(eY) += Tank[t]->GetY()*Tank[t]->GetContents();
-// vXYZtank(eZ) += Tank[t]->GetZ()*Tank[t]->GetContents();
-//
-// Tw += Tank[t]->GetContents();
-// }
-
- vXYZcg = (vXYZtank + EmptyWeight*vbaseXYZcg) / (Tw + EmptyWeight);
-
- // Calculate new moments of inertia here
-
- IXXt = IYYt = IZZt = IXZt = 0.0;
-// for (t=0; t<numTanks; t++) {
-// IXXt += ((Tank[t]->GetX()-vXYZcg(eX))/12.0)*((Tank[t]->GetX() - vXYZcg(eX))/12.0)*Tank[t]->GetContents()/GRAVITY;
-// IYYt += ((Tank[t]->GetY()-vXYZcg(eY))/12.0)*((Tank[t]->GetY() - vXYZcg(eY))/12.0)*Tank[t]->GetContents()/GRAVITY;
-// IZZt += ((Tank[t]->GetZ()-vXYZcg(eZ))/12.0)*((Tank[t]->GetZ() - vXYZcg(eZ))/12.0)*Tank[t]->GetContents()/GRAVITY;
-// IXZt += ((Tank[t]->GetX()-vXYZcg(eX))/12.0)*((Tank[t]->GetZ() - vXYZcg(eZ))/12.0)*Tank[t]->GetContents()/GRAVITY;
-// }
-
- Ixx = baseIxx + IXXt;
- Iyy = baseIyy + IYYt;
- Izz = baseIzz + IZZt;
- Ixz = baseIxz + IXZt;
-
-}
-
-//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-
-void FGAircraft::FMAero(void) {
- static FGColumnVector vDXYZcg(3);
- static FGColumnVector vAeroBodyForces(3);
- unsigned int axis_ctr,ctr;
-
- for (axis_ctr=1; axis_ctr<=3; axis_ctr++) vFs(axis_ctr) = 0.0;
-
- for (axis_ctr = 0; axis_ctr < 3; axis_ctr++) {
- for (ctr=0; ctr < Coeff[axis_ctr].size(); ctr++) {
- vFs(axis_ctr+1) += Coeff[axis_ctr][ctr]->TotalValue();
- }
- }
-
- vAeroBodyForces = State->GetTs2b(alpha, beta)*vFs;
- vForces += vAeroBodyForces;
-
- // see http://home.earthlink.net/~apeden/jsbsim_moments_due_to_forces.txt
- // for details on this
- vDXYZcg(eX) = -(vXYZrp(eX) - vXYZcg(eX))/12.0; //cg and rp values are in inches
- vDXYZcg(eY) = (vXYZrp(eY) - vXYZcg(eY))/12.0;
- vDXYZcg(eZ) = -(vXYZrp(eZ) - vXYZcg(eZ))/12.0;
-
- vMoments(eL) += vAeroBodyForces(eZ)*vDXYZcg(eY) - vAeroBodyForces(eY)*vDXYZcg(eZ); // rolling moment
- vMoments(eM) += vAeroBodyForces(eX)*vDXYZcg(eZ) - vAeroBodyForces(eZ)*vDXYZcg(eX); // pitching moment
- vMoments(eN) += vAeroBodyForces(eY)*vDXYZcg(eX) - vAeroBodyForces(eX)*vDXYZcg(eY); // yawing moment
-
- for (axis_ctr = 0; axis_ctr < 3; axis_ctr++) {
- for (ctr = 0; ctr < Coeff[axis_ctr+3].size(); ctr++) {
- vMoments(axis_ctr+1) += Coeff[axis_ctr+3][ctr]->TotalValue();
- }
- }
+void FGAircraft::FMAero(void)
+{
+ vForces += Aerodynamics->GetForces();
+ vMoments += Aerodynamics->GetMoments();
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-void FGAircraft::FMGear(void) {
-
+void FGAircraft::FMGear(void)
+{
if ( !GearUp ) {
vector <FGLGear>::iterator iGear = lGear.begin();
while (iGear != lGear.end()) {
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-void FGAircraft::FMMass(void) {
- vForces(eX) += -GRAVITY*sin(vEuler(eTht)) * Mass;
- vForces(eY) += GRAVITY*sin(vEuler(ePhi))*cos(vEuler(eTht)) * Mass;
- vForces(eZ) += GRAVITY*cos(vEuler(ePhi))*cos(vEuler(eTht)) * Mass;
+void FGAircraft::FMMass(void)
+{
+ vForces += Inertial->GetForces();
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-void FGAircraft::FMProp(void) {
- vForces += Propulsion->GetForces();
- vMoments += Propulsion->GetMoments();
+void FGAircraft::FMProp(void)
+{
+ vForces += Propulsion->GetForces();
+ vMoments += Propulsion->GetMoments();
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-void FGAircraft::GetState(void) {
+void FGAircraft::GetState(void)
+{
dt = State->Getdt();
alpha = Translation->Getalpha();
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-void FGAircraft::ReadMetrics(FGConfigFile* AC_cfg) {
+void FGAircraft::ReadMetrics(FGConfigFile* AC_cfg)
+{
string token = "";
string parameter;
+ float EW, bixx, biyy, bizz, bixz, biyz;
+ FGColumnVector vbaseXYZcg(3);
AC_cfg->GetNextConfigLine();
- while ((token = AC_cfg->GetValue()) != string("/METRICS")) {
+ while ((token = AC_cfg->GetValue()) != "/METRICS") {
*AC_cfg >> parameter;
- if (parameter == string("AC_WINGAREA")) {
- *AC_cfg >> WingArea;
- cout << " WingArea: " << WingArea << endl;
+ if (parameter == "AC_WINGAREA") {
+ *AC_cfg >> WingArea;
+ if (debug_lvl > 0) cout << " WingArea: " << WingArea << endl;
} else if (parameter == "AC_WINGSPAN") {
- *AC_cfg >> WingSpan;
- cout << " WingSpan: " << WingSpan << endl;
+ *AC_cfg >> WingSpan;
+ if (debug_lvl > 0) cout << " WingSpan: " << WingSpan << endl;
} else if (parameter == "AC_CHORD") {
- *AC_cfg >> cbar;
- cout << " Chord: " << cbar << endl;
+ *AC_cfg >> cbar;
+ if (debug_lvl > 0) cout << " Chord: " << cbar << endl;
} else if (parameter == "AC_IXX") {
- *AC_cfg >> baseIxx;
- cout << " baseIxx: " << baseIxx << endl;
+ *AC_cfg >> bixx;
+ if (debug_lvl > 0) cout << " baseIxx: " << bixx << endl;
+ MassBalance->SetBaseIxx(bixx);
} else if (parameter == "AC_IYY") {
- *AC_cfg >> baseIyy;
- cout << " baseIyy: " << baseIyy << endl;
- } else if (parameter == "AC_IZZ") {
- *AC_cfg >> baseIzz;
- cout << " baseIzz: " << baseIzz << endl;
- } else if (parameter == "AC_IXZ") {
- *AC_cfg >> baseIxz;
- cout << " baseIxz: " << baseIxz << endl;
+ *AC_cfg >> biyy;
+ if (debug_lvl > 0) cout << " baseIyy: " << biyy << endl;
+ MassBalance->SetBaseIyy(biyy);
+ } else if (parameter == "AC_IZZ") {
+ *AC_cfg >> bizz;
+ if (debug_lvl > 0) cout << " baseIzz: " << bizz << endl;
+ MassBalance->SetBaseIzz(bizz);
+ } else if (parameter == "AC_IXZ") {
+ *AC_cfg >> bixz;
+ if (debug_lvl > 0) cout << " baseIxz: " << bixz << endl;
+ MassBalance->SetBaseIxz(bixz);
+ } else if (parameter == "AC_IYZ") {
+ *AC_cfg >> biyz;
+ if (debug_lvl > 0) cout << " baseIyz: " << biyz << endl;
+ MassBalance->SetBaseIyz(biyz);
} else if (parameter == "AC_EMPTYWT") {
- *AC_cfg >> EmptyWeight;
- cout << " EmptyWeight: " << EmptyWeight << endl;
+ *AC_cfg >> EW;
+ MassBalance->SetEmptyWeight(EW);
+ if (debug_lvl > 0) cout << " EmptyWeight: " << EW << endl;
} else if (parameter == "AC_CGLOC") {
- *AC_cfg >> vbaseXYZcg(eX) >> vbaseXYZcg(eY) >> vbaseXYZcg(eZ);
- cout << " CG (x, y, z): " << vbaseXYZcg << endl;
+ *AC_cfg >> vbaseXYZcg(eX) >> vbaseXYZcg(eY) >> vbaseXYZcg(eZ);
+ MassBalance->SetBaseCG(vbaseXYZcg);
+ if (debug_lvl > 0) cout << " CG (x, y, z): " << vbaseXYZcg << endl;
} else if (parameter == "AC_EYEPTLOC") {
- *AC_cfg >> vXYZep(eX) >> vXYZep(eY) >> vXYZep(eZ);
- cout << " Eyepoint (x, y, z): " << vXYZep << endl;
+ *AC_cfg >> vXYZep(eX) >> vXYZep(eY) >> vXYZep(eZ);
+ if (debug_lvl > 0) cout << " Eyepoint (x, y, z): " << vXYZep << endl;
} else if (parameter == "AC_AERORP") {
- *AC_cfg >> vXYZrp(eX) >> vXYZrp(eY) >> vXYZrp(eZ);
- cout << " Ref Pt (x, y, z): " << vXYZrp << endl;
+ *AC_cfg >> vXYZrp(eX) >> vXYZrp(eY) >> vXYZrp(eZ);
+ if (debug_lvl > 0) cout << " Ref Pt (x, y, z): " << vXYZrp << endl;
} else if (parameter == "AC_ALPHALIMITS") {
- *AC_cfg >> alphaclmin >> alphaclmax;
- cout << " Maximum Alpha: " << alphaclmax
- << " Minimum Alpha: " << alphaclmin
+ *AC_cfg >> alphaclmin >> alphaclmax;
+ if (debug_lvl > 0) cout << " Maximum Alpha: " << alphaclmax
+ << " Minimum Alpha: " << alphaclmin
<< endl;
- }
+ }
}
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
void FGAircraft::ReadPropulsion(FGConfigFile* AC_cfg) {
- if (!Propulsion->LoadPropulsion(AC_cfg)) {
+ if (!Propulsion->Load(AC_cfg)) {
cerr << "Propulsion not successfully loaded" << endl;
}
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
void FGAircraft::ReadFlightControls(FGConfigFile* AC_cfg) {
- if (!FCS->LoadFCS(AC_cfg)) {
+ if (!FCS->Load(AC_cfg)) {
cerr << "Flight Controls not successfully loaded" << endl;
}
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-void FGAircraft::ReadAerodynamics(FGConfigFile* AC_cfg) {
- string token, axis;
-
- AC_cfg->GetNextConfigLine();
-
- while ((token = AC_cfg->GetValue()) != string("/AERODYNAMICS")) {
- if (token == "AXIS") {
- CoeffArray ca;
- axis = AC_cfg->GetValue("NAME");
- AC_cfg->GetNextConfigLine();
- while ((token = AC_cfg->GetValue()) != string("/AXIS")) {
- ca.push_back(new FGCoefficient(FDMExec, AC_cfg));
- DisplayCoeffFactors(ca.back()->Getmultipliers());
- }
- Coeff[AxisIdx[axis]]=ca;
- AC_cfg->GetNextConfigLine();
- }
+void FGAircraft::ReadAerodynamics(FGConfigFile* AC_cfg)
+{
+ if (!Aerodynamics->Load(AC_cfg)) {
+ cerr << "Aerodynamics not successfully loaded" << endl;
}
+
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
AC_cfg->GetNextConfigLine();
- while ((token = AC_cfg->GetValue()) != string("/UNDERCARRIAGE")) {
+ while ((token = AC_cfg->GetValue()) != "/UNDERCARRIAGE") {
lGear.push_back(FGLGear(AC_cfg, FDMExec));
}
}
Output->SetType(token);
AC_cfg->GetNextConfigLine();
- while ((token = AC_cfg->GetValue()) != string("/OUTPUT")) {
+ while ((token = AC_cfg->GetValue()) != "/OUTPUT") {
*AC_cfg >> parameter;
if (parameter == "RATE_IN_HZ") *AC_cfg >> OutRate;
if (parameter == "SIMULATION") {
*AC_cfg >> parameter;
if (parameter == "ON") subsystems += ssFCS;
}
+ if (parameter == "PROPULSION") {
+ *AC_cfg >> parameter;
+ if (parameter == "ON") subsystems += ssPropulsion;
+ }
}
Output->SetSubsystems(subsystems);
string token = AC_cfg->GetValue();
string scratch;
AircraftName = AC_cfg->GetValue("NAME");
- cout << underon << "Reading Aircraft Configuration File" << underoff << ": "
- << highint << AircraftName << normint << endl;
+ 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");
- cout << " Version: " << highint << CFGVersion
- << normint << endl;
- if (CFGVersion != string(NEEDED_CFG_VERSION)) {
- cout << endl << fgred << "YOU HAVE AN INCOMPATIBLE CFG FILE FOR THIS AIRCRAFT."
- " RESULTS WILL BE UNPREDICTABLE !!" << endl;
- cout << "Current version needed is: " << NEEDED_CFG_VERSION << endl;
- cout << " You have version: " << CFGVersion << endl << fgdef << endl;
- //exit(-1);
- }
-
-
-}
-
-//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-
-void FGAircraft::DisplayCoeffFactors(vector <eParam> multipliers) {
- cout << " Non-Dimensionalized by: ";
-
- for (unsigned int i=0; i<multipliers.size();i++)
- cout << State->paramdef[multipliers[i]];
- cout << endl;
-}
-
-//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-
-string FGAircraft::GetCoefficientStrings(void) {
- string CoeffStrings = "";
- bool firstime = true;
-
- for (unsigned int axis = 0; axis < 6; axis++) {
- for (unsigned int sd = 0; sd < Coeff[axis].size(); sd++) {
- if (firstime) {
- firstime = false;
- } else {
- CoeffStrings += ", ";
- }
- CoeffStrings += Coeff[axis][sd]->Getname();
- }
- }
-
- return CoeffStrings;
-}
-
-//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-
-string FGAircraft::GetCoefficientValues(void) {
- string SDValues = "";
- char buffer[10];
- bool firstime = true;
-
- for (unsigned int axis = 0; axis < 6; axis++) {
- for (unsigned int sd = 0; sd < Coeff[axis].size(); sd++) {
- if (firstime) {
- firstime = false;
- } else {
- SDValues += ", ";
- }
- sprintf(buffer, "%9.6f", Coeff[axis][sd]->GetSD());
- SDValues += string(buffer);
- }
+ if (debug_lvl > 0)
+ cout << " Version: " << highint << CFGVersion
+ << normint << endl;
+ 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 SDValues;
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
projects / flightgear.git / blobdiff