Andreas Gaeb: fix #222 (JSBSIm reset problems)

[flightgear.git] / src / FDM / JSBSim / models / FGAuxiliary.h

diff --git a/src/FDM/JSBSim/models/FGAuxiliary.h b/src/FDM/JSBSim/models/FGAuxiliary.h
index e551f5e3dd319ce85754f9eaddc48300555c0405..8f78212455db5896300e547ded4670caa8b7c8af 100644 (file)
--- a/src/FDM/JSBSim/models/FGAuxiliary.h
+++ b/src/FDM/JSBSim/models/FGAuxiliary.h
@@ -4,7 +4,7 @@
  Author:       Jon Berndt
  Date started: 01/26/99
 
- ------------- Copyright (C) 1999  Jon S. Berndt (jsb@hal-pc.org) -------------
+ ------------- Copyright (C) 1999  Jon S. Berndt (jon@jsbsim.org) -------------
 
  This program is free software; you can redistribute it and/or modify it under
  the terms of the GNU Lesser General Public License as published by the Free Software
@@ -40,15 +40,14 @@ INCLUDES
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
 
 #include "FGModel.h"
-#include <math/FGColumnVector3.h>
-#include <math/FGLocation.h>
-#include "FGPropagate.h"
+#include "math/FGColumnVector3.h"
+#include "math/FGLocation.h"
 
 /*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 DEFINITIONS
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
 
-#define ID_AUXILIARY "$Id$"
+#define ID_AUXILIARY "$Id: FGAuxiliary.h,v 1.19 2010/11/18 12:38:06 jberndt Exp $"
 
 /*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 FORWARD DECLARATIONS
@@ -100,7 +99,7 @@ CLASS DOCUMENTATION
     The radius R is calculated below in the vector vToEyePt.
 
     @author Tony Peden, Jon Berndt
-    @version $Id$
+    @version $Id: FGAuxiliary.h,v 1.19 2010/11/18 12:38:06 jberndt Exp $
 */
 
 /*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
@@ -162,7 +161,7 @@ public:
   const FGColumnVector3& GetAeroUVW    (void) const { return vAeroUVW;     }
   const FGLocation&      GetLocationVRP(void) const { return vLocationVRP; }
 
-  double GethVRP(void) const { return vLocationVRP.GetRadius() - Propagate->GetSeaLevelRadius(); }
+  double GethVRP(void) const;
   double GetAeroUVW (int idx) const { return vAeroUVW(idx); }
   double Getalpha   (void) const { return alpha;      }
   double Getbeta    (void) const { return beta;       }
@@ -171,24 +170,38 @@ public:
   double GetMagBeta (void) const { return fabs(beta); }
 
   double Getalpha   (int unit) const { if (unit == inDegrees) return alpha*radtodeg;
-                                       else cerr << "Bad units" << endl; return 0.0;}
+                                       else return BadUnits(); }
   double Getbeta    (int unit) const { if (unit == inDegrees) return beta*radtodeg;
-                                       else cerr << "Bad units" << endl; return 0.0;}
+                                       else return BadUnits(); }
   double Getadot    (int unit) const { if (unit == inDegrees) return adot*radtodeg;
-                                       else cerr << "Bad units" << endl; return 0.0;}
+                                       else return BadUnits(); }
   double Getbdot    (int unit) const { if (unit == inDegrees) return bdot*radtodeg;
-                                       else cerr << "Bad units" << endl; return 0.0;}
+                                       else return BadUnits(); }
   double GetMagBeta (int unit) const { if (unit == inDegrees) return fabs(beta)*radtodeg;
-                                       else cerr << "Bad units" << endl; return 0.0;}
+                                       else return BadUnits(); }
 
-  double Getqbar    (void) const { return qbar;       }
-  double GetqbarUW  (void) const { return qbarUW;     }
-  double GetqbarUV  (void) const { return qbarUV;     }
-  double GetVt      (void) const { return Vt;         }
-  double GetVground (void) const { return Vground;    }
-  double GetMach    (void) const { return Mach;       }
-  double GetMachU   (void) const { return MachU;      }
-  double GetNz      (void) const { return Nz;         }
+  double Getqbar          (void) const { return qbar;       }
+  double GetqbarUW        (void) const { return qbarUW;     }
+  double GetqbarUV        (void) const { return qbarUV;     }
+  double GetReynoldsNumber(void) const { return Re;         }
+
+  /** Gets the magnitude of total vehicle velocity including wind effects in feet per second. */
+  double GetVt            (void) const { return Vt;         }
+
+  /** Gets the ground speed in feet per second.
+      The magnitude is the square root of the sum of the squares (RSS) of the 
+      vehicle north and east velocity components.
+      @return The magnitude of the vehicle velocity in the horizontal plane. */
+  double GetVground       (void) const { return Vground;    }
+
+  /** Gets the Mach number. */
+  double GetMach          (void) const { return Mach;       }
+
+  /** The mach number calculated using the vehicle X axis velocity. */
+  double GetMachU         (void) const { return MachU;      }
+
+  /** The vertical acceleration in g's of the aircraft center of gravity. */
+  double GetNz            (void) const { return Nz;         }
 
   double GetHOverBCG(void) const { return hoverbcg; }
   double GetHOverBMAC(void) const { return hoverbmac; }
@@ -247,6 +260,7 @@ private:
 
   double Vt, Vground, Mach, MachU;
   double qbar, qbarUW, qbarUV;
+  double Re; // Reynolds Number = V*c/mu
   double alpha, beta;
   double adot,bdot;
   double psigt, gamma;
@@ -265,6 +279,7 @@ private:
   void CalculateRelativePosition(void);
 
   void bind(void);
+  double BadUnits(void) const;
   void Debug(int from);
 };