Member variable initialization fixes from Cameron Moore
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e0fa2db2c9
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8 changed files with 18 additions and 4 deletions
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@ -71,6 +71,7 @@ FGAerodynamics::FGAerodynamics(FGFDMExec* FDMExec) : FGModel(FDMExec)
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alphahystmin = alphahystmax = 0.0;
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clsq = lod = 0.0;
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alphaw = 0.0;
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bi2vel = ci2vel = 0.0;
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bind();
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Debug(0);
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@ -106,6 +106,7 @@ FGAircraft::FGAircraft(FGFDMExec* fdmex) : FGModel(fdmex)
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HTailArm = VTailArm = 0.0;
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lbarh = lbarv = 0.0;
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vbarh = vbarv = 0.0;
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WingIncidence = 0.0;
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bind();
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@ -83,6 +83,7 @@ FGCoefficient::FGCoefficient( FGFDMExec* fdex )
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totalValue = 0.0;
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bias = 0.0;
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gain = 1.0;
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SD = 0.0;
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filename.erase();
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description.erase();
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@ -115,6 +115,8 @@ FGFDMExec::FGFDMExec(FGPropertyManager* root)
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modelLoaded = false;
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IsSlave = false;
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cout << "FGFDMExec::FGFDMExec, FDMctr: " << FDMctr << endl;
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IdFDM = FDMctr;
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FDMctr++;
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@ -130,7 +132,6 @@ FGFDMExec::FGFDMExec(FGPropertyManager* root)
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else master = root;
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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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@ -156,7 +157,8 @@ FGFDMExec::~FGFDMExec()
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for (unsigned int i=1; i<SlaveFDMList.size(); i++) delete SlaveFDMList[i]->exec;
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SlaveFDMList.clear();
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cout << "FGFDMExec::~FGFDMExec, FDMctr: " << FDMctr << endl;
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FDMctr--;
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Debug(1);
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}
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@ -52,6 +52,12 @@ CLASS IMPLEMENTATION
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FGMassBalance::FGMassBalance(FGFDMExec* fdmex) : FGModel(fdmex)
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{
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Name = "FGMassBalance";
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Weight = EmptyWeight = Mass = 0.0;
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Ixx = Iyy = Izz = Ixy = Ixz = 0.0;
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baseIxx = baseIyy = baseIzz = baseIxy = baseIxz = 0.0;
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vbaseXYZcg(eX) = 0.0;
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vbaseXYZcg(eY) = 0.0;
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vbaseXYZcg(eZ) = 0.0;
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bind();
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Debug(0);
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@ -82,6 +82,8 @@ FGTranslation::FGTranslation(FGFDMExec* fdmex) : FGModel(fdmex)
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{
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Name = "FGTranslation";
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qbar = 0;
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qbarUW = 0.0;
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qbarUV = 0.0;
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Vt = 0.0;
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Mach = 0.0;
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alpha = beta = 0.0;
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@ -79,7 +79,7 @@ FGTrim::FGTrim(FGFDMExec *FDMExec,FGInitialCondition *FGIC, TrimMode tt ) {
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gamma_fallback=true;
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axis_count=0;
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mode=tt;
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xlo=xhi=alo=ahi;
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xlo=xhi=alo=ahi=0.0;
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targetNlf=1.0;
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debug_axis=tAll;
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switch(mode) {
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@ -57,6 +57,7 @@ FGKinemat::FGKinemat(FGFCS* fcs, FGConfigFile* AC_cfg) : FGFCSComponent(fcs),
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TransitionTimes.clear();
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OutputPct=0;
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InTransit=0;
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Type = AC_cfg->GetValue("TYPE");
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Name = AC_cfg->GetValue("NAME");
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