FORWARD DECLARATIONS
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
-/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-COMMENTS, REFERENCES, and NOTES [use "class documentation" below for API docs]
-%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+namespace JSBSim {
-%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
CLASS DOCUMENTATION
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
the Engines, Tanks, Propellers, Nozzles, Aerodynamic and Mass properties,
landing gear, etc. These constituent parts may actually run as separate
JSBSim models themselves, but the responsibility for initializing them and
- for retrieving their force and moment contributions falls to FGAircraft.<br>
-
+ for retrieving their force and moment contributions falls to FGAircraft.
@author Jon S. Berndt
@version $Id$
- @see
- <ol><li>Cooke, Zyda, Pratt, and McGhee, "NPSNET: Flight Simulation Dynamic Modeling
+ @see Cooke, Zyda, Pratt, and McGhee, "NPSNET: Flight Simulation Dynamic Modeling
Using Quaternions", Presence, Vol. 1, No. 4, pp. 404-420 Naval Postgraduate
- School, January 1994</li>
- <li>D. M. Henderson, "Euler Angles, Quaternions, and Transformation Matrices",
- JSC 12960, July 1977</li>
- <li>Richard E. McFarland, "A Standard Kinematic Model for Flight Simulation at
- NASA-Ames", NASA CR-2497, January 1975</li>
- <li>Barnes W. McCormick, "Aerodynamics, Aeronautics, and Flight Mechanics",
- Wiley & Sons, 1979 ISBN 0-471-03032-5</li>
- <li>Bernard Etkin, "Dynamics of Flight, Stability and Control", Wiley & Sons,
- 1982 ISBN 0-471-08936-2</li></ol>
+ School, January 1994
+ @see D. M. Henderson, "Euler Angles, Quaternions, and Transformation Matrices",
+ JSC 12960, July 1977
+ @see Richard E. McFarland, "A Standard Kinematic Model for Flight Simulation at
+ NASA-Ames", NASA CR-2497, January 1975
+ @see Barnes W. McCormick, "Aerodynamics, Aeronautics, and Flight Mechanics",
+ Wiley & Sons, 1979 ISBN 0-471-03032-5
+ @see Bernard Etkin, "Dynamics of Flight, Stability and Control", Wiley & Sons,
+ 1982 ISBN 0-471-08936-2
*/
/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
inline FGColumnVector3& GetForces(void) { return vForces; }
inline double GetForces(int idx) const { return vForces(idx); }
inline FGColumnVector3& GetBodyAccel(void) { return vBodyAccel; }
+ inline double GetBodyAccel(int idx) { return vBodyAccel(idx); }
inline FGColumnVector3& GetNcg (void) { return vNcg; }
+ inline double GetNcg(int idx) { return vNcg(idx); }
inline FGColumnVector3& GetXYZrp(void) { return vXYZrp; }
+ inline FGColumnVector3& GetXYZvrp(void) { return vXYZvrp; }
inline FGColumnVector3& GetXYZep(void) { return vXYZep; }
inline double GetXYZrp(int idx) const { return vXYZrp(idx); }
+ inline double GetXYZvrp(int idx) const { return vXYZvrp(idx); }
inline double GetXYZep(int idx) const { return vXYZep(idx); }
- inline double GetAlphaCLMax(void) const { return alphaclmax; }
- inline double GetAlphaCLMin(void) const { return alphaclmin; }
-
- inline void SetAlphaCLMax(double tt) { alphaclmax=tt; }
- inline void SetAlphaCLMin(double tt) { alphaclmin=tt; }
inline void SetAircraftName(string name) {AircraftName = name;}
-
- inline double GetStallWarn(void) const { return impending_stall; }
-
- double GetBI2Vel(void) const { return bi2vel; }
- double GetCI2Vel(void) const { return ci2vel; }
- double GetAlphaW(void) const { return alphaw; }
-
-
+
float GetNlf(void);
-
+
inline FGColumnVector3& GetNwcg(void) { return vNwcg; }
-
+
void bind(void);
void unbind(void);
FGColumnVector3 vMoments;
FGColumnVector3 vForces;
FGColumnVector3 vXYZrp;
+ FGColumnVector3 vXYZvrp;
FGColumnVector3 vXYZep;
FGColumnVector3 vEuler;
FGColumnVector3 vDXYZcg;
double WingArea, WingSpan, cbar, WingIncidence;
double HTailArea, VTailArea, HTailArm, VTailArm;
double lbarh,lbarv,vbarh,vbarv;
- double alphaclmax,alphaclmin;
- double impending_stall;
- double bi2vel, ci2vel,alphaw;
string AircraftName;
void Debug(int from);
};
+} // namespace JSBSim
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
#endif