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
-
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
CLASS DOCUMENTATION
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
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).
+
@author Jon S. Berndt
@version $Id$
@see
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>
+ @see <a href="http://cvs.sourceforge.net/cgi-bin/viewcvs.cgi/jsbsim/JSBSim/FGAircraft.h?rev=HEAD&content-type=text/vnd.viewcvs-markup">
+ Header File </a>
+ @see <a href="http://cvs.sourceforge.net/cgi-bin/viewcvs.cgi/jsbsim/JSBSim/FGAircraft.cpp?rev=HEAD&content-type=text/vnd.viewcvs-markup">
+ Source File </a>
*/
/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
inline string GetAircraftName(void) { return AircraftName; }
/// Gets the wing area
- inline double GetWingArea(void) { return WingArea; }
+ double GetWingArea(void) const { return WingArea; }
/// Gets the wing span
- inline double GetWingSpan(void) { return WingSpan; }
+ double GetWingSpan(void) const { return WingSpan; }
/// Gets the average wing chord
- inline double Getcbar(void) { return cbar; }
- inline double GetWingIncidence(void) { return WingIncidence; }
- inline double GetHTailArea(void) { return HTailArea; }
- inline double GetHTailArm(void) { return HTailArm; }
- inline double GetVTailArea(void) { return VTailArea; }
- inline double GetVTailArm(void) { return VTailArm; }
- inline double Getlbarh(void) { return lbarh; } // HTailArm / cbar
- inline double Getlbarv(void) { return lbarv; } // VTailArm / cbar
- inline double Getvbarh(void) { return vbarh; } // H. Tail Volume
- inline double 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 FGColumnVector3& GetNcg (void) { return vNcg; }
+ inline FGColumnVector3& GetNcg (void) { return vNcg; }
inline FGColumnVector3& GetXYZrp(void) { return vXYZrp; }
inline FGColumnVector3& GetXYZep(void) { return vXYZep; }
- inline double GetXYZrp(int idx) { return vXYZrp(idx); }
- inline double GetXYZep(int idx) { return vXYZep(idx); }
- inline double GetAlphaCLMax(void) { return alphaclmax; }
- inline double GetAlphaCLMin(void) { return alphaclmin; }
+ inline double GetXYZrp(int idx) const { return vXYZrp(idx); }
+ inline double GetXYZep(int idx) const { return vXYZep(idx); }
+ inline void SetAircraftName(string name) {AircraftName = name;}
- inline void SetAlphaCLMax(double tt) { alphaclmax=tt; }
- inline void SetAlphaCLMin(double tt) { alphaclmin=tt; }
-
- inline double GetStallWarn(void) { return impending_stall; }
-
float GetNlf(void);
-
+
inline FGColumnVector3& GetNwcg(void) { return vNwcg; }
+ void bind(void);
+ void unbind(void);
+
private:
FGColumnVector3 vMoments;
FGColumnVector3 vForces;
double WingArea, WingSpan, cbar, WingIncidence;
double HTailArea, VTailArea, HTailArm, VTailArm;
double lbarh,lbarv,vbarh,vbarv;
- double alphaclmax,alphaclmin;
- double impending_stall;
- string CFGVersion;
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);
};
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
projects / flightgear.git / blobdiff