MappingMeanOsculatingOrbitElements.h

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/*! \file MappingMeanOsculatingOrbitElements.h
*  \brief First order mapping algorithm between mean orbit elments and osculating orbit elements. 
*       Referenced from "Anayltic Mechanics of Space Systems" by Schaub and Junkins (p.693).
*  \author $Author: jayhawk_hokie $
*  \version $Revision: 1.2 $
*  \date    $Date: 2007/08/31 16:52:10 $
*//////////////////////////////////////////////////////////////////////////////////////////////////
/*
* 
*/
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#ifndef __MEAN_OSCULATING_ORBIT_ELEMENTS_H__
#define __MEAN_OSCULATING_ORBIT_ELEMENTS_H__

#include <iostream>
#include "rotation/Rotation.h"
#include "Keplerian.h"

using namespace std;

namespace O_SESSAME 
{

/*! \brief Keplerian Osculating and Mean orbital element representation of the orbital position.
 * \ingroup OrbitStateRepresentation
 *
 * The OsculatingOrbitalElement class stores the Osculating or Mean orbital elements of an orbital position using the Keplerian Class.
 *
 *      \par Example:
 *
 */

        class OsculatingOrbitalElements : public Keplerian
        {
                public:
                        virtual ~OsculatingOrbitalElements();

                        virtual OsculatingOrbitalElements* NewPointer();

                        virtual OsculatingOrbitalElements* Clone();

                                OsculatingOrbitalElements();

                        void SetOsculatingOrbitalElements( Keplerian& _OsculatingOrbitalElements );

                        void SetOsculatingOrbitalElements( CAMdoubleVector _ECIVector );

                        void SetMeanOrbitalElements( Keplerian& _MeanOrbitalElements );

                        void SetMeanOrbitalElements( CAMdoubleVector _ECIVector );

                        Keplerian GetMeanOrbitalElements( );

                        Keplerian GetOsculatingOrbitalElements( );
                        
                        void OsculatingToMean( );
                        
                        void MeanToOsculating( );

                        Keplerian Mapping( Keplerian& _keplerian );



                private:
                        Keplerian m_OsculatingOrbitalElements;
                
                        Keplerian m_MeanOrbitalElements;
                
                        double m_Gamma2;

        };      


} // end O_SESSAME


#endif

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