Z:/work/code/expcfidev/cplusplusWrapper/Lib/include/StateVector.h

//--------------------------------------------------------
// Earth Observation Mission CFI Software. Version 4.5
//--------------------------------------------------------

//--------------------------------------------------------------------
// CVS Info: $Id: StateVector.h,v 1.12 2013-02-05 11:22:02 expcfi Exp $ 
//--------------------------------------------------------------------

#ifndef _EECFI_STATEVECTOR_H
#define _EECFI_STATEVECTOR_H


//--INCLUDE-----------------------------------------------------------
#include "LibData.h"
#include "CfiClass.h"
#include "CfiError.h"
#include "EETime.h"
#include "Coord.h"
#include "ModelId.h"

//--NAMESPACES-------------------------------------------------------- 
using namespace std;

namespace EECFI
{

  class StateVector: public CfiClass
  {
    public:

      Time   time;   
      Coord  coord;  

      StateVector() {};

      StateVector(Time &time, Coord &coord);

      ~StateVector() {};

      StateVector change( const ModelId &modelId, long deriv, long newCS) throw (CfiError);

      void setSun( const ModelId &modelId, Time &time) throw (CfiError);

      void setMoon( const ModelId &modelId, Time &time) throw (CfiError);

      void setPlanet( const ModelId &modelId, Time &time, long planet) throw (CfiError);

      //  The latitude angle is the angle between the satellite position and the intersection of the orbital plane with a given reference plane.
      void getPositionOnOrbit( const ModelId &modelId, 
                               long angleType, long deriv, 
                               double &angle,
                               double &angleRate,
                               double &angleRateRate) throw (CfiError);
    protected:

    private:

  };
  
} // closing namespace

#endif