#endif
#include "FGModel.h"
-#include "FGPropulsion.h"
#include "FGConfigFile.h"
-#include "FGMatrix33.h"
#include "FGColumnVector3.h"
-#include "FGColumnVector4.h"
-#include "FGLGear.h"
/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
DEFINITIONS
FORWARD DECLARATIONS
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
-/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-COMMENTS, REFERENCES, and NOTES [use "class documentation" below for API docs]
-%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-
-Longitudinal
- CL0 - Reference lift at zero alpha
- CD0 - Reference drag at zero alpha
- CDM - Drag due to Mach
- CLa - Lift curve slope (w.r.t. alpha)
- CDa - Drag curve slope (w.r.t. alpha)
- CLq - Lift due to pitch rate
- CLM - Lift due to Mach
- CLadt - Lift due to alpha rate
-
- Cmadt - Pitching Moment due to alpha rate
- Cm0 - Reference Pitching moment at zero alpha
- Cma - Pitching moment slope (w.r.t. alpha)
- Cmq - Pitch damping (pitch moment due to pitch rate)
- CmM - Pitch Moment due to Mach
-
-Lateral
- Cyb - Side force due to sideslip
- Cyr - Side force due to yaw rate
-
- Clb - Dihedral effect (roll moment due to sideslip)
- Clp - Roll damping (roll moment due to roll rate)
- Clr - Roll moment due to yaw rate
- Cnb - Weathercocking stability (yaw moment due to sideslip)
- Cnp - Rudder adverse yaw (yaw moment due to roll rate)
- Cnr - Yaw damping (yaw moment due to yaw rate)
-
-Control
- CLDe - Lift due to elevator
- CDDe - Drag due to elevator
- CyDr - Side force due to rudder
- CyDa - Side force due to aileron
-
- CmDe - Pitch moment due to elevator
- ClDa - Roll moment due to aileron
- ClDr - Roll moment due to rudder
- CnDr - Yaw moment due to rudder
- CnDa - Yaw moment due to aileron
+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>
- When an aircraft model is loaded the config file is parsed and for each of the
- sections of the config file (propulsion, flight control, etc.) the
- corresponding "ReadXXX()" method is called. From within this method the
- "Load()" method of that system is called (e.g. LoadFCS).
+ 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 string GetAircraftName(void) { return AircraftName; }
/// Gets the wing area
- inline float GetWingArea(void) { return WingArea; }
+ double GetWingArea(void) const { return WingArea; }
/// Gets the wing span
- inline float GetWingSpan(void) { return WingSpan; }
+ double GetWingSpan(void) const { return WingSpan; }
/// Gets the average wing chord
- inline float Getcbar(void) { return cbar; }
- inline float GetWingIncidence(void) { return WingIncidence; }
- inline float GetHTailArea(void) { return HTailArea; }
- inline float GetHTailArm(void) { return HTailArm; }
- inline float GetVTailArea(void) { return VTailArea; }
- inline float GetVTailArm(void) { return VTailArm; }
- inline float Getlbarh(void) { return lbarh; } // HTailArm / cbar
- inline float Getlbarv(void) { return lbarv; } // VTailArm / cbar
- inline float Getvbarh(void) { return vbarh; } // H. Tail Volume
- inline float Getvbarv(void) { return vbarv; } // V. Tail Volume
+ double Getcbar(void) const { return cbar; }
+ inline double GetWingIncidence(void) const { return WingIncidence; }
+ inline double GetHTailArea(void) const { return HTailArea; }
+ inline double GetHTailArm(void) const { return HTailArm; }
+ inline double GetVTailArea(void) const { return VTailArea; }
+ inline double GetVTailArm(void) const { return VTailArm; }
+ inline double Getlbarh(void) const { return lbarh; } // HTailArm / cbar
+ inline double Getlbarv(void) const { return lbarv; } // VTailArm / cbar
+ inline double Getvbarh(void) const { return vbarh; } // H. Tail Volume
+ inline double Getvbarv(void) const { return vbarv; } // V. Tail Volume
inline FGColumnVector3& GetMoments(void) { return vMoments; }
+ inline double GetMoments(int idx) const { return vMoments(idx); }
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 float GetXYZrp(int idx) { return vXYZrp(idx); }
- inline float GetXYZep(int idx) { return vXYZep(idx); }
- inline float GetAlphaCLMax(void) { return alphaclmax; }
- inline float GetAlphaCLMin(void) { return alphaclmin; }
-
- inline void SetAlphaCLMax(float tt) { alphaclmax=tt; }
- inline void SetAlphaCLMin(float tt) { alphaclmin=tt; }
-
- /// Subsystem types for specifying which will be output in the FDM data logging
- enum SubSystems {
- /** Subsystem: Simulation (= 1) */ ssSimulation = 1,
- /** Subsystem: Aerosurfaces (= 2) */ ssAerosurfaces = 2,
- /** Subsystem: Body rates (= 4) */ ssRates = 4,
- /** Subsystem: Velocities (= 8) */ ssVelocities = 8,
- /** Subsystem: Forces (= 16) */ ssForces = 16,
- /** Subsystem: Moments (= 32) */ ssMoments = 32,
- /** Subsystem: Atmosphere (= 64) */ ssAtmosphere = 64,
- /** Subsystem: Mass Properties (= 128) */ ssMassProps = 128,
- /** Subsystem: Coefficients (= 256) */ ssCoefficients = 256,
- /** Subsystem: Position (= 512) */ ssPosition = 512,
- /** Subsystem: Ground Reactions (= 1024) */ ssGroundReactions = 1024,
- /** Subsystem: FCS (= 2048) */ ssFCS = 2048,
- /** Subsystem: Propulsion (= 4096) */ ssPropulsion = 4096
- } subsystems;
+ 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 void SetAircraftName(string name) {AircraftName = name;}
+
+ float GetNlf(void);
+
+ inline FGColumnVector3& GetNwcg(void) { return vNwcg; }
+
+ void bind(void);
+ void unbind(void);
private:
FGColumnVector3 vMoments;
FGColumnVector3 vForces;
FGColumnVector3 vXYZrp;
+ FGColumnVector3 vXYZvrp;
FGColumnVector3 vXYZep;
- FGColumnVector3 vEuler;
FGColumnVector3 vDXYZcg;
FGColumnVector3 vBodyAccel;
- float WingArea, WingSpan, cbar, WingIncidence;
- float HTailArea, VTailArea, HTailArm, VTailArm;
- float lbarh,lbarv,vbarh,vbarv;
- float alphaclmax,alphaclmin;
- string CFGVersion;
+ FGColumnVector3 vNcg;
+ FGColumnVector3 vNwcg;
+
+ double WingArea, WingSpan, cbar, WingIncidence;
+ double HTailArea, VTailArea, HTailArm, VTailArm;
+ double lbarh,lbarv,vbarh,vbarv;
string AircraftName;
- void ReadMetrics(FGConfigFile*);
- void ReadPropulsion(FGConfigFile*);
- void ReadFlightControls(FGConfigFile*);
- void ReadAerodynamics(FGConfigFile*);
- void ReadUndercarriage(FGConfigFile*);
- void ReadPrologue(FGConfigFile*);
- void ReadOutput(FGConfigFile*);
- void Debug(void);
+ void Debug(int from);
};
+} // namespace JSBSim
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
#endif
projects / flightgear.git / blobdiff