X-Git-Url: https://git.mxchange.org/?a=blobdiff_plain;f=src%2FFDM%2FJSBSim%2Fmodels%2FFGPropulsion.cpp;h=32d8b42a1df129d58b4b7f022b926f9d6a9107f7;hb=c5c895dae250898d667ae29641c51a550be7ee90;hp=e71dfeaf03d11cc9dcb0fb8e017801a3a6b075a1;hpb=13ec36af4218402eda39c680e8da6ca2c198733c;p=flightgear.git diff --git a/src/FDM/JSBSim/models/FGPropulsion.cpp b/src/FDM/JSBSim/models/FGPropulsion.cpp index e71dfeaf0..32d8b42a1 100644 --- a/src/FDM/JSBSim/models/FGPropulsion.cpp +++ b/src/FDM/JSBSim/models/FGPropulsion.cpp @@ -45,7 +45,6 @@ INCLUDES %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/ #include "FGPropulsion.h" -#include "FGState.h" #include "models/FGFCS.h" #include "models/FGMassBalance.h" #include "models/propulsion/FGThruster.h" @@ -66,7 +65,7 @@ using namespace std; namespace JSBSim { -static const char *IdSrc = "$Id$"; +static const char *IdSrc = "$Id: FGPropulsion.cpp,v 1.43 2010/11/18 12:38:06 jberndt Exp $"; static const char *IdHdr = ID_PROPULSION; extern short debug_lvl; @@ -116,6 +115,8 @@ FGPropulsion::~FGPropulsion() bool FGPropulsion::InitModel(void) { + bool result = true; + if (!FGModel::InitModel()) return false; for (unsigned int i=0; iResetToIC(); @@ -124,18 +125,28 @@ bool FGPropulsion::InitModel(void) switch (Engines[i]->GetType()) { case FGEngine::etPiston: ((FGPiston*)Engines[i])->ResetToIC(); - if (HasInitializedEngines && (InitializedEngines & i)) InitRunning(i); + try { + if (HasInitializedEngines && (InitializedEngines & i)) InitRunning(i); + } catch (string str) { + cerr << str << endl; + result = false; + } break; case FGEngine::etTurbine: ((FGTurbine*)Engines[i])->ResetToIC(); - if (HasInitializedEngines && (InitializedEngines & i)) InitRunning(i); + try { + if (HasInitializedEngines && (InitializedEngines & i)) InitRunning(i); + } catch (string str) { + cerr << str << endl; + result = false; + } break; default: break; } } - return true; + return result; } //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% @@ -149,7 +160,7 @@ bool FGPropulsion::Run(void) RunPreFunctions(); - double dt = State->Getdt(); + double dt = FDMExec->GetDeltaT(); vForces.InitMatrix(); vMoments.InitMatrix(); @@ -227,14 +238,13 @@ bool FGPropulsion::GetSteadyState(void) void FGPropulsion::InitRunning(int n) { - if (n > 0) { // A specific engine is supposed to be initialized + if (n >= 0) { // A specific engine is supposed to be initialized if (n >= (int)GetNumEngines() ) { - cerr << "Tried to initialize a non-existent engine!" << endl; - throw; + throw(string("Tried to initialize a non-existent engine!")); } - FCS->SetThrottleCmd(n,1); - FCS->SetMixtureCmd(n,1); + FDMExec->GetFCS()->SetThrottleCmd(n,1); + FDMExec->GetFCS()->SetMixtureCmd(n,1); GetEngine(n)->InitRunning(); GetSteadyState(); @@ -244,16 +254,14 @@ void FGPropulsion::InitRunning(int n) } else if (n < 0) { // -1 refers to "All Engines" for (unsigned int i=0; iSetThrottleCmd(i,1); - FCS->SetMixtureCmd(i,1); + FDMExec->GetFCS()->SetThrottleCmd(i,1); + FDMExec->GetFCS()->SetMixtureCmd(i,1); GetEngine(i)->InitRunning(); } GetSteadyState(); InitializedEngines = -1; HasInitializedEngines = true; - } else if (n == 0) { // No engines are to be initialized - // Do nothing } } @@ -296,32 +304,37 @@ bool FGPropulsion::Load(Element* el) document->SetParent(engine_element); type = document->GetName(); - if (type == "piston_engine") { - HavePistonEngine = true; - if (!IsBound) bind(); - Engines.push_back(new FGPiston(FDMExec, document, numEngines)); - } else if (type == "turbine_engine") { - HaveTurbineEngine = true; - if (!IsBound) bind(); - Engines.push_back(new FGTurbine(FDMExec, document, numEngines)); - } else if (type == "turboprop_engine") { - HaveTurboPropEngine = true; - if (!IsBound) bind(); - Engines.push_back(new FGTurboProp(FDMExec, document, numEngines)); - } else if (type == "rocket_engine") { - HaveRocketEngine = true; - if (!IsBound) bind(); - Engines.push_back(new FGRocket(FDMExec, document, numEngines)); - } else if (type == "electric_engine") { - HaveElectricEngine = true; - if (!IsBound) bind(); - Engines.push_back(new FGElectric(FDMExec, document, numEngines)); - } else { - cerr << "Unknown engine type: " << type << endl; - exit(-5); + try { + if (type == "piston_engine") { + HavePistonEngine = true; + if (!IsBound) bind(); + Engines.push_back(new FGPiston(FDMExec, document, numEngines)); + } else if (type == "turbine_engine") { + HaveTurbineEngine = true; + if (!IsBound) bind(); + Engines.push_back(new FGTurbine(FDMExec, document, numEngines)); + } else if (type == "turboprop_engine") { + HaveTurboPropEngine = true; + if (!IsBound) bind(); + Engines.push_back(new FGTurboProp(FDMExec, document, numEngines)); + } else if (type == "rocket_engine") { + HaveRocketEngine = true; + if (!IsBound) bind(); + Engines.push_back(new FGRocket(FDMExec, document, numEngines)); + } else if (type == "electric_engine") { + HaveElectricEngine = true; + if (!IsBound) bind(); + Engines.push_back(new FGElectric(FDMExec, document, numEngines)); + } else { + cerr << "Unknown engine type: " << type << endl; + exit(-5); + } + } catch (std::string str) { + cerr << endl << fgred << str << reset << endl; + return false; } - FCS->AddThrottle(); + FDMExec->GetFCS()->AddThrottle(); ThrottleAdded = true; numEngines++; @@ -331,13 +344,13 @@ bool FGPropulsion::Load(Element* el) } CalculateTankInertias(); - if (!ThrottleAdded) FCS->AddThrottle(); // need to have at least one throttle + if (!ThrottleAdded) FDMExec->GetFCS()->AddThrottle(); // need to have at least one throttle // Process fuel dump rate if (el->FindElement("dump-rate")) DumpRate = el->FindElementValueAsNumberConvertTo("dump-rate", "LBS/MIN"); - FGModel::PostLoad(el); + PostLoad(el, PropertyManager); return true; } @@ -397,7 +410,7 @@ ifstream* FGPropulsion::FindEngineFile(const string& engine_filename) //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% -string FGPropulsion::GetPropulsionStrings(const string& delimiter) +string FGPropulsion::GetPropulsionStrings(const string& delimiter) const { unsigned int i; @@ -421,7 +434,7 @@ string FGPropulsion::GetPropulsionStrings(const string& delimiter) //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% -string FGPropulsion::GetPropulsionValues(const string& delimiter) +string FGPropulsion::GetPropulsionValues(const string& delimiter) const { unsigned int i; @@ -479,7 +492,7 @@ FGMatrix33& FGPropulsion::CalculateTankInertias(void) tankJ = FGMatrix33(); for (unsigned int i=0; iGetPointmassInertia( lbtoslug * Tanks[i]->GetContents(), + tankJ += FDMExec->GetMassBalance()->GetPointmassInertia( lbtoslug * Tanks[i]->GetContents(), Tanks[i]->GetXYZ() ); tankJ(1,1) += Tanks[i]->GetIxx(); tankJ(2,2) += Tanks[i]->GetIyy();