OrbitController.h

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//////////////////////////////////////////////////////////////////////////////////////////////////
/*! \file: OrbitController.h
*  \brief: Orbit Element Controller for DSACSS.
*  \author $Author: jayhawk_hokie $
*  \version $Revision: 1.1 $
*  \date    $Date: 2007/08/31 15:58:35 $
*//////////////////////////////////////////////////////////////////////////////////////////////////
/*! 
*/
//////////////////////////////////////////////////////////////////////////////////////////////////

#ifndef __ORBIT_CONTROLLER_H__
#define __ORBIT_CONTROLLER_H__

#include <stdlib.h>
#include <unistd.h>
#include <string.h>
#include <stdio.h>
#include <iostream.h>

// Standard Includes
#include <rotation/Rotation.h>
#include <matrix/Matrix.h>

// Orbit Includes
#include <orbit/Orbit.h>
#include <orbit/OrbitState.h>
#include <orbit/orbitstaterep/Keplerian.h>

#include <Base/Whorl.h>

// transform coe
#include <orbit/orbitstaterep/MappingMeanOsculatingOrbitElements.h>

#include "Sensors/AshtechG12_GPS_PhysicalDevice.h"
#include "Sensors/AccelerationClient.h"

using namespace std;
using namespace O_SESSAME;

// this is not a good solution.... fix later
// The number of satellites that Geode has been compiled for.
static const int                        MASS            =100;    //  to be specified in main program (kg)

class OrbitController 
{

        public:
                OrbitController( );

                virtual ~OrbitController( );

                // Facilitators

                        // Mutators

                                /*! Runs the observer (pure virtual function) */
                                virtual int Run() = 0;

                                /*! Initializes the observer (pure virtual function */
                                virtual int Initialize() = 0;

                CAMdoubleMatrix DirectionCosMatrix1Axis( double _angle );

                CAMdoubleMatrix DirectionCosMatrix2Axis( double _angle );

                CAMdoubleMatrix DirectionCosMatrix3Axis( double _angle );

                CAMdoubleVector WGS2ECEFPosition( double _latitude, double _longitude, double _altitude );

                CAMdoubleVector NED2ECEFVelocity( double _latitude, double _longitude, double _altitude, 
                double _velocityNorth, double _velocityEast, double _velocityDown );

                CAMdoubleVector WGS842ECEF( double _latitude, double _longitude, double _altitude, 
                double _velocityNorth, double _velocityEast, double _velocityDown );

                CAMdoubleVector ECEFPosition2WGS84( double _x, double _y, double _z );

                CAMdoubleVector ECEF2NEDVelocity( double _latitude, double _longitude, double _altitude, 
                double _Vx, double _Vy, double _Vz );

                CAMdoubleVector ECEF2WGS84( double _x, double _y, double _z, double _Vx, double _Vy, double _Vz );

                CAMdoubleVector ECEF2ECI( CAMdoubleVector _ECEFVector, double _jDay );

                CAMdoubleVector ECI2ECEF( CAMdoubleVector _ECIVector, double _jDay );

                double lat_lon( double latlon, char sector );

                void TangentPlaneState( AshtechG12_GPS_PhysicalDevice::Position recPos, CAMdoubleVector &_WGS84Vector );


                Vector thruster(Vector udesired);

                void cals(Vector ECI, Vector VECI, double a, double& H, double& p, double& b, double& r);

                void ECI2COE(Vector ECI, Vector VECI, Keplerian& myCOE, double& a, double& e, double& i, double& Lon, double& Arg, double& tru); 

        protected:

                /*! \brief Member object in Controller Class */
                Whorl* m_whorl;

                /* Space Vehicle Id */
                int m_vehicleID ;

                /* Acceleration Duration [s] */
                double m_duration;

                /* Space Vehicle Mass [kg] */
                double m_mass;

                /* Current Time */
                ssfTime m_vehicleTime;

                /* Reset delta V time history from orbit propagator */
                AccelerationMessage * m_accelerationVector;

};

#endif

// Do not change the comments below - they will be added automatically by CVS
/*****************************************************************************
*       $Log: OrbitController.h,v $
*       Revision 1.1  2007/08/31 15:58:35  jayhawk_hokie
*       Initial Submission.
*
*       
*
******************************************************************************/

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