AttitudeModels.h

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//////////////////////////////////////////////////////////////////////////////////////////////////
/*! \file AttitudeModels.h
 *  \brief Class for various spacecraft attitude models
 *  \author $Author: jayhawk_hokie $
 *  \version $Revision: 1.1 $
 *  \date    $Date: 2007/06/19 19:55:08 $
*//////////////////////////////////////////////////////////////////////////////////////////////////
/*!
*/
//////////////////////////////////////////////////////////////////////////////////////////////////


#ifndef __SSSL_ATTITUDEMODELS_H__
#define __SSSL_ATTITUDEMODELS_H__


#include "attitude/Attitude.h"
#include "attitude/AttitudeState.h"

#include "rotation/Rotation.h"

#include "matrix/Matrix.h"

using namespace std;
using namespace O_SESSAME;

class AttitudeModels 
{
        public:
                /*! \brief Constructors */
                AttitudeModels( );

                /*! \brief Destructor */
                virtual ~AttitudeModels( );

                /*! \brief MRP Kinematic Expression
                 *  @param _mrp attitude representation
                 *  @param _angularVelocity [rad/s]
                 *  @return _mrpRate [rad/s]
                 */
                void MRPKinematic(  ModifiedRodriguezParameters _mrp, Vector _angularVelocity, ModifiedRodriguezParameters &_mrpRate );
                
                /*! \brief Quaternion Kinematic Expression
                 *  @param _quaternion attitude representation
                 *  @param _angularVelocity [rad/s]
                 *  @return _quaternionRate [rad/s]
                 */
                void QuaternionKinematic(  Quaternion _quaternion, Vector _angularVelocity, Quaternion &_quaternionRate );

        protected:

        private: 

};

#endif

// Do not change the comments below - they will be added automatically by CVS
/*****************************************************************************
*       $Log: AttitudeModels.h,v $
*       Revision 1.1  2007/06/19 19:55:08  jayhawk_hokie
*       Initial submission. Added MRP and Quaternion Kinematic Equations.
*
*
*
*
******************************************************************************/

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