]> git.mxchange.org Git - flightgear.git/blobdiff - src/FDM/JSBSim/FGState.cpp
Updated to match changes in radiostack.[ch]xx
[flightgear.git] / src / FDM / JSBSim / FGState.cpp
index 3359a85498d0d7747a39ccff9a65aba0e922428c..f76e5d027bb2cf6a9140d2bced6ed891fde5dc66 100644 (file)
@@ -60,9 +60,6 @@ static const char *IdHdr = ID_STATE;
 MACROS
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
 
-//#define RegisterVariable(ID,DEF) coeffdef[#ID] = ID; paramdef[ID] = DEF
-#define RegisterVariable(ID,DEF) coeffdef[#ID] = ID;
-
 /*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 CLASS IMPLEMENTATION
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
@@ -233,8 +230,8 @@ void FGState::Initialize(double U, double V, double W,
 
 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
-void FGState::Initialize(FGInitialCondition *FGIC) {
-
+void FGState::Initialize(FGInitialCondition *FGIC)
+{
   double tht,psi,phi;
   double U, V, W, h;
   double latitude, longitude;
@@ -263,7 +260,8 @@ void FGState::Initialize(FGInitialCondition *FGIC) {
 
 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
-void FGState::InitMatrices(double phi, double tht, double psi) {
+void FGState::InitMatrices(double phi, double tht, double psi)
+{
   double thtd2, psid2, phid2;
   double Sthtd2, Spsid2, Sphid2;
   double Cthtd2, Cpsid2, Cphid2;
@@ -299,7 +297,8 @@ void FGState::InitMatrices(double phi, double tht, double psi) {
 
 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
-void FGState::CalcMatrices(void) {
+void FGState::CalcMatrices(void)
+{
   double Q0Q0, Q1Q1, Q2Q2, Q3Q3;
   double Q0Q1, Q0Q2, Q0Q3, Q1Q2;
   double Q1Q3, Q2Q3;
@@ -331,7 +330,8 @@ void FGState::CalcMatrices(void) {
 
 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
-void FGState::IntegrateQuat(FGColumnVector3 vPQR, int rate) {
+void FGState::IntegrateQuat(FGColumnVector3 vPQR, int rate)
+{
   vQdot(1) = -0.5*(vQtrn(2)*vPQR(eP) + vQtrn(3)*vPQR(eQ) + vQtrn(4)*vPQR(eR));
   vQdot(2) =  0.5*(vQtrn(1)*vPQR(eP) + vQtrn(3)*vPQR(eR) - vQtrn(4)*vPQR(eQ));
   vQdot(3) =  0.5*(vQtrn(1)*vPQR(eQ) + vQtrn(4)*vPQR(eP) - vQtrn(2)*vPQR(eR));
@@ -345,7 +345,8 @@ void FGState::IntegrateQuat(FGColumnVector3 vPQR, int rate) {
 
 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
-FGColumnVector3& FGState::CalcEuler(void) {
+FGColumnVector3& FGState::CalcEuler(void)
+{
   if (mTl2b(3,3) == 0.0) mTl2b(3,3) = 0.0000001;
   if (mTl2b(1,1) == 0.0) mTl2b(1,1) = 0.0000001;
 
@@ -427,16 +428,18 @@ void FGState::ReportState(void)
                    FDMExec->GetMassBalance()->GetXYZcg(2),
                    FDMExec->GetMassBalance()->GetXYZcg(3));
   cout << out;             
-  if( FCS->GetDfPos() <= 0.01)
+  if ( FCS->GetDfPos() <= 0.01)
     snprintf(flap,10,"Up");
   else
     snprintf(flap,10,"%2.0f",FCS->GetDfPos());
-  if(FCS->GetGearPos() < 0.01)
+
+  if (FCS->GetGearPos() < 0.01)
     snprintf(gear,12,"Up");
-  else if(FCS->GetGearPos() > 0.99)
+  else if (FCS->GetGearPos() > 0.99)
     snprintf(gear,12,"Down");
   else
-    snprintf(gear,12,"In Transit");   
+    snprintf(gear,12,"In Transit");
+
   snprintf(out,80, "    Flaps: %3s  Gear: %12s\n",flap,gear);
   cout << out;
   snprintf(out,80, "    Speed: %4.0f KCAS  Mach: %5.2f\n",
@@ -491,9 +494,12 @@ void FGState::ReportState(void)
 
 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
-void FGState::InitPropertyMaps(void)  {
+void FGState::InitPropertyMaps(void)
+{
   ParamNameToProp[  "FG_TIME" ]="sim-time-sec";
   ParamNameToProp[  "FG_QBAR" ]="aero/qbar-psf";
+  ParamNameToProp[  "FG_QBARUW" ]="aero/qbarUW-psf";
+  ParamNameToProp[  "FG_QBARUV" ]="aero/qbarUV-psf";
   ParamNameToProp[  "FG_WINGAREA" ]="metrics/Sw-sqft";
   ParamNameToProp[  "FG_WINGSPAN" ]="metrics/bw-ft";
   ParamNameToProp[  "FG_CBAR" ]="metrics/cbarw-ft";
@@ -568,24 +574,24 @@ void FGState::InitPropertyMaps(void)  {
   ParamNameToProp[  "FG_VBARV" ]="metrics/vbarv-norm";     
   ParamNameToProp[  "FG_GEAR_CMD" ]="gear/gear-cmd-norm";
   ParamNameToProp[  "FG_GEAR_POS" ]="gear/gear-pos-norm";
-  
+  ParamNameToProp[  "FG_HYSTPARM" ]="aero/stall-hyst-norm";
 }
 
 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
-void FGState::bind(void) {
+void FGState::bind(void)
+{
   PropertyManager->Tie("sim-time-sec",this,
                         &FGState::Getsim_time);
 }
 
 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
                         
-void FGState::unbind(void) {
+void FGState::unbind(void)
+{
   PropertyManager->Untie("sim-time-sec");
 }
 
-
-
 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 //    The bitmasked value choices are as follows:
 //    unset: In this case (the default) JSBSim would only print
@@ -632,4 +638,3 @@ void FGState::Debug(int from)
   }
 }
 
-