- FGColumnVector3& GetvLastFs(void) { return vLastFs; }
- double GetvLastFs(int axis) const { return vLastFs(axis); }
- FGColumnVector3& GetvFs(void) { return vFs; }
- double GetvFs(int axis) const { return vFs(axis); }
- inline double GetLoD(void) const { return lod; }
- inline double GetClSquared(void) const { return clsq; }
- inline double GetAlphaCLMax(void) const { return alphaclmax; }
- inline double GetAlphaCLMin(void) const { return alphaclmin; }
-
- inline double GetAlphaHystMax(void) const { return alphahystmax; }
- inline double GetAlphaHystMin(void) const { return alphahystmin; }
- inline double GetHysteresisParm(void) const { return stall_hyst; }
- inline double GetStallWarn(void) const { return impending_stall; }
+ /** Retrieves the aerodynamic forces in the wind axes.
+ @return a reference to a column vector containing the wind axis forces. */
+ const FGColumnVector3& GetvFw(void) const { return vFw; }
+
+ /** Retrieves the aerodynamic forces in the wind axes, given an axis.
+ @param axis the axis to return the force for (eX, eY, eZ).
+ @return a reference to a column vector containing the requested wind
+ axis force. */
+ double GetvFw(int axis) const { return vFw(axis); }
+
+ /** Retrieves the lift over drag ratio */
+ double GetLoD(void) const { return lod; }
+
+ /** Retrieves the square of the lift coefficient. */
+ double GetClSquared(void) const { return clsq; }
+ double GetAlphaCLMax(void) const { return alphaclmax; }
+ double GetAlphaCLMin(void) const { return alphaclmin; }
+
+ double GetHysteresisParm(void) const { return stall_hyst; }
+ double GetStallWarn(void) const { return impending_stall; }