Fix stall widths for the "auxilliary" (reverse flow) stalls so they

[flightgear.git] / src / FDM / JSBSim / FGPropagate.h

diff --git a/src/FDM/JSBSim/FGPropagate.h b/src/FDM/JSBSim/FGPropagate.h
index 420876774d0a2aaef58c16f822a551fdd349da0f..b778bb096b03ead058aa2705a4e17c4e1c703395 100644 (file)
--- a/src/FDM/JSBSim/FGPropagate.h
+++ b/src/FDM/JSBSim/FGPropagate.h
@@ -106,7 +106,9 @@ public:
   double Geth(void)   const { return VState.vLocation.GetRadius() - SeaLevelRadius; }
   double GetPQR(int axis) const {return VState.vPQR(axis);}
   double GetPQRdot(int idx) const {return vPQRdot(idx);}
-  double GetEuler(int axis) const { return VState.vQtrn.GetEuler()(axis); }
+  double GetEuler(int axis) const { return VState.vQtrn.GetEuler(axis); }
+  double GetCosEuler(int idx) const { return VState.vQtrn.GetCosEuler(idx); }
+  double GetSinEuler(int idx) const { return VState.vQtrn.GetSinEuler(idx); }
   double Gethdot(void) const { return -vVel(eDown); }
 
   /** Returns the "constant" RunwayRadius.
@@ -114,26 +116,14 @@ public:
       zero if JSBSim is running in standalone mode.
       @return distance of the runway from the center of the earth.
       @units feet */
-  double GetRunwayRadius(void) const { return RunwayRadius; }
+  double GetRunwayRadius(void) const;
   double GetSeaLevelRadius(void) const { return SeaLevelRadius; }
-  double GetDistanceAGL(void)  const { return VState.vLocation.GetRadius()-RunwayRadius; }
+  double GetDistanceAGL(void)  const;
   double GetRadius(void) const { return VState.vLocation.GetRadius(); }
   double GetLongitude(void) const { return VState.vLocation.GetLongitude(); }
   double GetLatitude(void) const { return VState.vLocation.GetLatitude(); }
   const FGLocation& GetLocation(void) const { return VState.vLocation; }
 
-  double Getphi(void) const { return VState.vQtrn.GetEulerPhi(); }
-  double Gettht(void) const { return VState.vQtrn.GetEulerTheta(); }
-  double Getpsi(void) const { return VState.vQtrn.GetEulerPsi(); }
-
-  double GetCosphi(void) const { return VState.vQtrn.GetCosEulerPhi(); }
-  double GetCostht(void) const { return VState.vQtrn.GetCosEulerTheta(); }
-  double GetCospsi(void) const { return VState.vQtrn.GetCosEulerPsi(); }
-
-  double GetSinphi(void) const { return VState.vQtrn.GetSinEulerPhi(); }
-  double GetSintht(void) const { return VState.vQtrn.GetSinEulerTheta(); }
-  double GetSinpsi(void) const { return VState.vQtrn.GetSinEulerPsi(); }
-
   /** Retrieves the local-to-body transformation matrix.
       @return a reference to the local-to-body transformation matrix.  */
   const FGMatrix33& GetTl2b(void) const { return VState.vQtrn.GetT(); }
@@ -149,11 +139,12 @@ public:
   void SetRadius(double r) { VState.vLocation.SetRadius(r); }
   void SetLocation(const FGLocation& l) { VState.vLocation = l; }
   void Seth(double tt);
-  void SetRunwayRadius(double tt) { RunwayRadius = tt; }
   void SetSeaLevelRadius(double tt) { SeaLevelRadius = tt; }
   void SetDistanceAGL(double tt);
   void SetInitialState(const FGInitialCondition *);
 
+  void RecomputeRunwayRadius(void);
+
   void bind(void);
   void unbind(void);