OrbitObserver.h

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//////////////////////////////////////////////////////////////////////////////////////////////////
/*! \file: OrbitObserver.h
*  \brief: Orbit Element Observer for DSACSS.
*  \author $Author: jayhawk_hokie $
*  \version $Revision: 1.1 $
*  \date    $Date: 2007/08/31 16:09:30 $
*//////////////////////////////////////////////////////////////////////////////////////////////////
/*!
*/
//////////////////////////////////////////////////////////////////////////////////////////////////

#ifndef __ORBIT_OBSERVER_H__
#define __ORBIT_OBSERVER_H__

// System Includes
#include <stdlib.h>
#include <unistd.h>
#include <string.h>
#include <stdio.h>
#include <iostream.h>

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

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

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

// GPS Sensor
#include <Sensors/AshtechG12_GPS_PhysicalDevice.h>

// Simulator
#include<Base/Whorl.h>
//#include<Base/WhorlSim.h>

// Communication
#include "Comm/ClientSocket.h"
#include "Comm/SocketException.h"

// XML Parser
#include "dsacssinterface.h"

using namespace std;

using namespace O_SESSAME;


class OrbitObserver
{

        public:

                OrbitObserver( );

                virtual ~OrbitObserver( );

                // Facilitators

                        // Mutators

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

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


                Matrix DirectionCosMatrix1Axis( double _angle );

                Matrix DirectionCosMatrix2Axis( double _angle );

                Matrix DirectionCosMatrix3Axis( double _angle );

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

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

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

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

                Vector ECEF2NEDVelocity( double _latitude, double _longitude, double _altitude,
                        double _Vx, double _Vy, double _Vz );
                
                Vector ECEF2WGS84( double _x, double _y, double _z, double _Vx, double _Vy, double _Vz );

                Vector ECEF2ECI( CAMdoubleVector _ECEFVector, double _jDay );

                Vector ECI2ECEF( CAMdoubleVector _ECIVector, double _jDay );

                double lat_lon( double latlon, char sector );

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

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

        protected:

};

#endif

// Do not change the comments below - they will be added automatically by CVS
/*****************************************************************************
*       $Log: OrbitObserver.h,v $
*       Revision 1.1  2007/08/31 16:09:30  jayhawk_hokie
*       Initial Submission.
*
*
*
******************************************************************************/

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