Removed FGMatrix.* because it is no longer used by JSBSim.

[flightgear.git] / src / FDM / JSBSim / FGAircraft.h

diff --git a/src/FDM/JSBSim/FGAircraft.h b/src/FDM/JSBSim/FGAircraft.h
index 8dc7beb7c92532714af6e0ff5a545c16b49c9fd9..240d75259477cd2ef6a6dd9a4abeb9eaeb09b12c 100644 (file)
--- a/src/FDM/JSBSim/FGAircraft.h
+++ b/src/FDM/JSBSim/FGAircraft.h
@@ -74,45 +74,6 @@ 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
-
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 CLASS DOCUMENTATION
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
@@ -123,10 +84,7 @@ 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
@@ -199,6 +157,7 @@ public:
 
   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) { return impending_stall; }
   
@@ -222,17 +181,9 @@ private:
   double lbarh,lbarv,vbarh,vbarv;
   double alphaclmax,alphaclmin;
   double impending_stall;
-  string CFGVersion;
   string AircraftName;
 
-  bool ReadMetrics(FGConfigFile*);
-  bool ReadPropulsion(FGConfigFile*);
-  bool ReadFlightControls(FGConfigFile*);
-  bool ReadAerodynamics(FGConfigFile*);
-  bool ReadUndercarriage(FGConfigFile*);
-  bool ReadPrologue(FGConfigFile*);
-  bool ReadOutput(FGConfigFile*);
-  void Debug(void);
+  void Debug(int from);
 };
 
 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%