You should have received a copy of the GNU General Public License along with
this program; if not, write to the Free Software Foundation, Inc., 59 Temple
Place - Suite 330, Boston, MA 02111-1307, USA.
-
+
Further information about the GNU General Public License can also be found on
the world wide web at http://www.gnu.org.
#ifdef FGFS
# include <simgear/compiler.h>
-# ifdef FG_HAVE_STD_INCLUDES
+# ifdef SG_HAVE_STD_INCLUDES
# include <vector>
# include <iterator>
-# include <map>
# else
# include <vector.h>
# include <iterator.h>
-# include <map.h>
# endif
#else
# include <vector>
# include <iterator>
-# include <map>
#endif
#include "FGModel.h"
-#include "FGCoefficient.h"
-#include "FGEngine.h"
-#include "FGTank.h"
-#include "FGLGear.h"
+#include "FGPropulsion.h"
#include "FGConfigFile.h"
-#include "FGMatrix.h"
+#include "FGMatrix33.h"
+#include "FGColumnVector3.h"
+#include "FGColumnVector4.h"
+#include "FGLGear.h"
/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
DEFINITIONS
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
-#define ID_AIRCRAFT "$Header$"
+#define ID_AIRCRAFT "$Id$"
/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
FORWARD DECLARATIONS
/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
COMMENTS, REFERENCES, and NOTES [use "class documentation" below for API docs]
-%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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.
+ for retrieving their force and moment contributions falls to FGAircraft.<br>
+
@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>
*/
/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
class FGAircraft : public FGModel {
- enum {eL=1, eM, eN};
- enum {eX=1, eY, eZ};
- enum {eP=1, eQ, eR};
- enum {ePhi=1, eTht, ePsi};
-
public:
/** Constructor
@param Executive a pointer to the parent executive object */
FGAircraft(FGFDMExec *Executive);
/// Destructor
- ~FGAircraft(void);
+ ~FGAircraft();
/** Runs the Aircraft model; called by the Executive
@see JSBSim.cpp documentation
/** Loads the aircraft.
The executive calls this method to load the aircraft into JSBSim.
- @param apath path to the aircraft files (e.g. "aircraft/X15/")
- @param epath path to engine files (e.g. "engine/")
- @param acname name of aircraft (e.g. "X15")
- @return true if succesful */
- bool LoadAircraft(string apath, string epath, string acname);
+ @param AC_cfg a pointer to the config file instance
+ @return true if successful */
+ bool Load(FGConfigFile* AC_cfg);
/** Gets the aircraft name
@return the name of the aircraft as a string type */
inline string GetAircraftName(void) { return AircraftName; }
- /** Gets the gear status
- @return true if gear is not deployed */
- inline bool GetGearUp(void) { return GearUp; }
- /** Gets the number of gear units defined for the aircraft
- @return number of gear units defined */
- inline int GetNumGearUnits(void) { return lGear.size(); }
- /** Gets a gear instance
- @param gear index of gear instance
- @return a pointer to the FGLGear instance of the gear unit requested */
- inline FGLGear* GetGearUnit(int gear) { return &(lGear[gear]); }
/// 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; }
- /** Gets an engine instance.
- @param engine index of the engine instance
- @return a pointer to the FGEngine instance of the requested engine */
- inline FGEngine* GetEngine(int engine) { return Engine[engine]; }
- /** Gets a tank instance.
- @param tank index of the tank instance
- @return a pointer to the FGTank instance of the requested tank */
- inline FGTank* GetTank(int tank) { return Tank[tank]; }
- inline float GetWeight(void) { return Weight; }
- inline float GetMass(void) { return Mass; }
- inline FGColumnVector GetMoments(void) { return vMoments; }
- inline FGColumnVector GetForces(void) { return vForces; }
- inline FGColumnVector GetvFs(void) { return vFs; }
- inline float GetIxx(void) { return Ixx; }
- inline float GetIyy(void) { return Iyy; }
- inline float GetIzz(void) { return Izz; }
- inline float GetIxz(void) { return Ixz; }
- inline unsigned int GetNumEngines(void) { return numEngines; }
- inline FGColumnVector GetXYZcg(void) { return vXYZcg; }
- inline FGColumnVector GetXYZrp(void) { return vXYZrp; }
- inline FGColumnVector GetXYZep(void) { return vXYZep; }
- inline float GetNlf(void) { return nlf; }
- inline float GetAlphaCLMax(void) { return alphaclmax; }
- inline float GetAlphaCLMin(void) { return alphaclmin; }
-
- inline void SetGearUp(bool tt) { GearUp = tt; }
- inline void SetAlphaCLMax(float tt) { alphaclmax=tt; }
- inline void SetAlphaCLMin(float tt) { alphaclmin=tt; }
-
- inline FGCoefficient* GetCoeff(int axis, int idx) { return Coeff[axis][idx]; }
- string GetCoefficientStrings(void);
- string GetCoefficientValues(void);
- string GetGroundReactionStrings(void);
- string GetGroundReactionValues(void);
-
- /// 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
- } subsystems;
+ 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& GetXYZrp(void) { return vXYZrp; }
+ inline FGColumnVector3& GetXYZep(void) { return vXYZep; }
+ 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;}
+
+ float GetNlf(void);
+
+ inline FGColumnVector3& GetNwcg(void) { return vNwcg; }
+
+ void bind(void);
+ void unbind(void);
private:
- void GetState(void);
- void FMAero(void);
- void FMGear(void);
- void FMMass(void);
- void FMProp(void);
- void MassChange(void);
- FGColumnVector vMoments;
- FGColumnVector vForces;
- FGColumnVector vFs;
- FGColumnVector vXYZrp;
- FGColumnVector vbaseXYZcg;
- FGColumnVector vXYZcg;
- FGColumnVector vXYZep;
- FGColumnVector vEuler;
- float baseIxx, baseIyy, baseIzz, baseIxz, EmptyMass, Mass;
- float Ixx, Iyy, Izz, Ixz;
- float alpha, beta;
- float WingArea, WingSpan, cbar;
- float Weight, EmptyWeight;
- float nlf,alphaclmax,alphaclmin;
- float dt;
- string CFGVersion;
+ FGColumnVector3 vMoments;
+ FGColumnVector3 vForces;
+ FGColumnVector3 vXYZrp;
+ FGColumnVector3 vXYZep;
+ FGColumnVector3 vEuler;
+ FGColumnVector3 vDXYZcg;
+ FGColumnVector3 vBodyAccel;
+ FGColumnVector3 vNcg;
+ FGColumnVector3 vNwcg;
+
+ double WingArea, WingSpan, cbar, WingIncidence;
+ double HTailArea, VTailArea, HTailArm, VTailArm;
+ double lbarh,lbarv,vbarh,vbarv;
string AircraftName;
- unsigned int numTanks;
- unsigned int numEngines;
- unsigned int numSelectedOxiTanks;
- unsigned int numSelectedFuelTanks;
- FGTank* Tank[MAX_TANKS]; // need to make a vector
- FGEngine *Engine[MAX_ENGINES]; // need to make a vector
-
- typedef map<string,int> AxisIndex;
- AxisIndex AxisIdx;
-
- typedef vector<FGCoefficient*> CoeffArray;
-
- CoeffArray* Coeff;
-
- void DisplayCoeffFactors(vector <eParam> multipliers);
-
- bool GearUp;
-
- string Axis[6];
- vector <FGLGear> lGear;
-
- string AircraftPath;
- string EnginePath;
- void ReadMetrics(FGConfigFile*);
- void ReadPropulsion(FGConfigFile*);
- void ReadFlightControls(FGConfigFile*);
- void ReadAerodynamics(FGConfigFile*);
- void ReadUndercarriage(FGConfigFile*);
- void ReadPrologue(FGConfigFile*);
- void ReadOutput(FGConfigFile*);
+ void Debug(int from);
};
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
#endif
+
projects / flightgear.git / blobdiff