]> git.mxchange.org Git - flightgear.git/blobdiff - src/FDM/JSBSim/FGTrimAxis.h
Fix stall widths for the "auxilliary" (reverse flow) stalls so they
[flightgear.git] / src / FDM / JSBSim / FGTrimAxis.h
index 605bca53e52c5c0418baa8d72f18ba526150fa76..e0754a03ce22ba8cc5c0c21800bcee3434e6bc74 100644 (file)
@@ -44,10 +44,18 @@ INCLUDES
 #include "FGJSBBase.h"
 #include "FGInitialCondition.h"
 
+/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+DEFINITIONS
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
+
 #define ID_TRIMAXIS "$Id$"
 
 #define DEFAULT_TOLERANCE 0.001
 
+/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+FORWARD DECLARATIONS
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
+
 namespace JSBSim {
 
 const string StateNames[10]=   { "all","udot","vdot","wdot","qdot","pdot","rdot",
@@ -63,6 +71,13 @@ const string ControlNames[14]= { "Throttle","Sideslip","Angle of Attack",
 
 class FGInitialCondition;
 
+/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+CLASS DOCUMENTATION
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
+
+/** Models an aircraft axis for purposes of trimming.
+  */
+
 /*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 CLASS DECLARATION
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
@@ -120,8 +135,8 @@ public:
   void SetThetaOnGround(double ff);
   void SetPhiOnGround(double ff);
   
-  inline void SetStateTarget(float target) { state_target=target; }
-  inline float GetStateTarget(void) { return state_target; }
+  inline void SetStateTarget(double target) { state_target=target; }
+  inline double GetStateTarget(void) { return state_target; }
   
   bool initTheta(void);
   
@@ -136,10 +151,10 @@ private:
   State   state;
   Control control;
   
-  float state_target;
+  double state_target;
   
-  float state_value;
-  float control_value;
+  double state_value;
+  double control_value;
 
   double control_min;
   double control_max;