bool FGFDMExec::Allocate(void)
{
bool result=true;
Models.resize(eNumStandardModels);
// See the eModels enum specification in the header file. The order of the enums
// specifies the order of execution. The Models[] vector is the primary
// storage array for the list of models.
Models[ePropagate] = new FGPropagate(this);
Models[eInput] = new FGInput(this);
Models[eInertial] = new FGInertial(this);
Models[eAtmosphere] = new FGStandardAtmosphere(this);
Models[eWinds] = new FGWinds(this);
Models[eAuxiliary] = new FGAuxiliary(this);
Models[eSystems] = new FGFCS(this);
Models[ePropulsion] = new FGPropulsion(this);
Models[eAerodynamics] = new FGAerodynamics (this);
GetGroundCallback()->SetSeaLevelRadius(((FGInertial*)Models[eInertial])->GetRefRadius());
Models[eGroundReactions] = new FGGroundReactions(this);
Models[eExternalReactions] = new FGExternalReactions(this);
Models[eBuoyantForces] = new FGBuoyantForces(this);
Models[eMassBalance] = new FGMassBalance(this);
Models[eAircraft] = new FGAircraft(this);
Models[eAccelerations] = new FGAccelerations(this);
// Assign the Model shortcuts for internal executive use only.
Propagate = (FGPropagate*)Models[ePropagate];
Inertial = (FGInertial*)Models[eInertial];
Atmosphere = (FGAtmosphere*)Models[eAtmosphere];
Winds = (FGWinds*)Models[eWinds];
Auxiliary = (FGAuxiliary*)Models[eAuxiliary];
FCS = (FGFCS*)Models[eSystems];
Propulsion = (FGPropulsion*)Models[ePropulsion];
Aerodynamics = (FGAerodynamics*)Models[eAerodynamics];
GroundReactions = (FGGroundReactions*)Models[eGroundReactions];
ExternalReactions = (FGExternalReactions*)Models[eExternalReactions];
BuoyantForces = (FGBuoyantForces*)Models[eBuoyantForces];
MassBalance = (FGMassBalance*)Models[eMassBalance];
Aircraft = (FGAircraft*)Models[eAircraft];
Accelerations = (FGAccelerations*)Models[eAccelerations];
// Initialize planet (environment) constants
LoadPlanetConstants();
// Initialize models
for (unsigned int i = 0; i < Models.size(); i++) {
LoadInputs(i);
Models[i]->InitModel();
}
IC = new FGInitialCondition(this);
modelLoaded = false;
return result;
}
void FGFDMExec::LoadModelConstants(void)
{
Winds->in.wingspan = Aircraft->GetWingSpan();
FCS->in.NumGear = GroundReactions->GetNumGearUnits();
Aerodynamics->in.Wingarea = Aircraft->GetWingArea();
Aerodynamics->in.Wingchord = Aircraft->Getcbar();
Aerodynamics->in.Wingincidence = Aircraft->GetWingIncidence();
Aerodynamics->in.Wingspan = Aircraft->GetWingSpan();
Auxiliary->in.Wingspan = Aircraft->GetWingSpan();
Auxiliary->in.Wingchord = Aircraft->Getcbar();
GroundReactions->in.vXYZcg = MassBalance->GetXYZcg();
LoadPlanetConstants();
}
void FGFDMExec::LoadModelConstants(void)
{
Winds->in.wingspan = Aircraft->GetWingSpan();
FCS->in.NumGear = GroundReactions->GetNumGearUnits();
Aerodynamics->in.Wingarea = Aircraft->GetWingArea();
Aerodynamics->in.Wingchord = Aircraft->Getcbar();
Aerodynamics->in.Wingincidence = Aircraft->GetWingIncidence();
Aerodynamics->in.Wingspan = Aircraft->GetWingSpan();
Auxiliary->in.Wingspan = Aircraft->GetWingSpan();
Auxiliary->in.Wingchord = Aircraft->Getcbar();
for (int i=0; i<GroundReactions->GetNumGearUnits(); i++) {
GroundReactions->in.vWhlBodyVec[i] = MassBalance->StructuralToBody(GroundReactions->GetGearUnit(i)->GetLocation());
}
LoadPlanetConstants();
}
bool FGFDMExec::Allocate(void)
{
bool result=true;
Models.resize(eNumStandardModels);
// First build the inertial model since some other models are relying on
// the inertial model and the ground callback to build themselves.
// Note that this does not affect the order in which the models will be
// executed later.
Models[eInertial] = new FGInertial(this);
SetGroundCallback(new FGDefaultGroundCallback(static_cast<FGInertial*>(Models[eInertial])->GetRefRadius()));
// See the eModels enum specification in the header file. The order of the
// enums specifies the order of execution. The Models[] vector is the primary
// storage array for the list of models.
Models[ePropagate] = new FGPropagate(this);
Models[eInput] = new FGInput(this);
Models[eAtmosphere] = new FGStandardAtmosphere(this);
Models[eWinds] = new FGWinds(this);
Models[eSystems] = new FGFCS(this);
Models[eMassBalance] = new FGMassBalance(this);
Models[eAuxiliary] = new FGAuxiliary(this);
Models[ePropulsion] = new FGPropulsion(this);
Models[eAerodynamics] = new FGAerodynamics (this);
Models[eGroundReactions] = new FGGroundReactions(this);
Models[eExternalReactions] = new FGExternalReactions(this);
Models[eBuoyantForces] = new FGBuoyantForces(this);
Models[eAircraft] = new FGAircraft(this);
Models[eAccelerations] = new FGAccelerations(this);
Models[eOutput] = new FGOutput(this);
// Assign the Model shortcuts for internal executive use only.
Propagate = (FGPropagate*)Models[ePropagate];
Inertial = (FGInertial*)Models[eInertial];
Atmosphere = (FGAtmosphere*)Models[eAtmosphere];
Winds = (FGWinds*)Models[eWinds];
FCS = (FGFCS*)Models[eSystems];
MassBalance = (FGMassBalance*)Models[eMassBalance];
Auxiliary = (FGAuxiliary*)Models[eAuxiliary];
Propulsion = (FGPropulsion*)Models[ePropulsion];
Aerodynamics = (FGAerodynamics*)Models[eAerodynamics];
GroundReactions = (FGGroundReactions*)Models[eGroundReactions];
ExternalReactions = (FGExternalReactions*)Models[eExternalReactions];
BuoyantForces = (FGBuoyantForces*)Models[eBuoyantForces];
Aircraft = (FGAircraft*)Models[eAircraft];
Accelerations = (FGAccelerations*)Models[eAccelerations];
Output = (FGOutput*)Models[eOutput];
// Initialize planet (environment) constants
LoadPlanetConstants();
// Initialize models
for (unsigned int i = 0; i < Models.size(); i++) {
// The Input/Output models must not be initialized prior to IC loading
if (i == eInput || i == eOutput) continue;
LoadInputs(i);
Models[i]->InitModel();
}
IC = new FGInitialCondition(this);
IC->bind(instance);
modelLoaded = false;
return result;
}
