JSBSim updates.

[flightgear.git] / src / FDM / flight.hxx

diff --git a/src/FDM/flight.hxx b/src/FDM/flight.hxx
index 20fc9a6c60278afc5c1cfcd489b939b0b3b61e7e..efd04db45ea47bae6dd00feae40918db2183ca86 100644 (file)
--- a/src/FDM/flight.hxx
+++ b/src/FDM/flight.hxx
@@ -341,26 +341,30 @@ public:
     }
 
     FG_VECTOR_3    n_cg_body_v;
-    // inline double * get_N_cg_body_v() { return n_cg_body_v; }
-    // inline double get_N_X_cg() const { return n_cg_body_v[0]; }
-    // inline double get_N_Y_cg() const { return n_cg_body_v[1]; }
-    // inline double get_N_Z_cg() const { return n_cg_body_v[2]; }
-    /* inline void set_Accels_CG_Body_N( double x, double y, double z ) {
+     inline double * get_N_cg_body_v() { return n_cg_body_v; }
+     inline double get_N_X_cg() const { return n_cg_body_v[0]; }
+     inline double get_N_Y_cg() const { return n_cg_body_v[1]; }
+     inline double get_N_Z_cg() const { return n_cg_body_v[2]; }
+     inline void set_Accels_CG_Body_N( double x, double y, double z ) {
        n_cg_body_v[0] = x;
        n_cg_body_v[1] = y;
        n_cg_body_v[2] = z;
-    } */
+    } 
 
     FG_VECTOR_3    n_pilot_body_v;
     // inline double * get_N_pilot_body_v() { return n_pilot_body_v; }
-    // inline double get_N_X_pilot() const { return n_pilot_body_v[0]; }
-    // inline double get_N_Y_pilot() const { return n_pilot_body_v[1]; }
-    // inline double get_N_Z_pilot() const { return n_pilot_body_v[2]; }
-    /* inline void set_Accels_Pilot_Body_N( double x, double y, double z ) {
+    inline double get_N_X_pilot() const { return n_pilot_body_v[0]; }
+    inline double get_N_Y_pilot() const { return n_pilot_body_v[1]; }
+    inline double get_N_Z_pilot() const { return n_pilot_body_v[2]; }
+    inline void set_Accels_Pilot_Body_N( double x, double y, double z ) {
        n_pilot_body_v[0] = x;
        n_pilot_body_v[1] = y;
        n_pilot_body_v[2] = z;
-    } */
+    } 
+    
+    double nlf;  //Normal Load Factor
+    double get_Nlf(void) { return nlf; }  
+    void set_Nlf(double n) { nlf=n;  }
 
     FG_VECTOR_3    omega_dot_body_v;
     // inline double * get_Omega_dot_body_v() { return omega_dot_body_v; }
@@ -876,5 +880,3 @@ void fgFDMSetGroundElevation(int model, double alt_meters);
 
 
 #endif // _FLIGHT_HXX
-
-