DEFINITIONS
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
-#define ID_BUOYANTFORCES "$Id: FGBuoyantForces.h,v 1.15 2011/08/14 20:15:56 jberndt Exp $"
+#define ID_BUOYANTFORCES "$Id: FGBuoyantForces.h,v 1.16 2011/10/31 14:54:41 bcoconni Exp $"
/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
FORWARD DECLARATIONS
See FGGasCell for the full configuration file format for gas cells.
@author Anders Gidenstam, Jon S. Berndt
- @version $Id: FGBuoyantForces.h,v 1.15 2011/08/14 20:15:56 jberndt Exp $
+ @version $Id: FGBuoyantForces.h,v 1.16 2011/10/31 14:54:41 bcoconni Exp $
*/
/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
/** Gets the total gas mass. The gas mass is part of the aircraft's
inertia.
@return mass in slugs. */
- double GetGasMass(void);
+ double GetGasMass(void) const;
/** Gets the total moment from the gas mass.
@return a moment vector in the structural frame in lbs in. */
/** Gets the strings for the current set of gas cells.
@param delimeter either a tab or comma string depending on output type
@return a string containing the descriptive names for all parameters */
- string GetBuoyancyStrings(string delimeter);
+ string GetBuoyancyStrings(const string& delimeter);
/** Gets the coefficient values.
@param delimeter either a tab or comma string depending on output type
@return a string containing the numeric values for the current set of
parameters */
- string GetBuoyancyValues(string delimeter);
+ string GetBuoyancyValues(const string& delimeter);
FGGasCell::Inputs in;