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# Z:/work/code/expcfidev/cplusplusWrapper/Pointing/include/Attitude.h

    00001 //--------------------------------------------------------
    00002 // Earth Observation Mission CFI Software. Version 4.4
    00003 //--------------------------------------------------------
    00004
    00005 //--------------------------------------------------------------------
    00006 // CVS Info: $Id: Attitude.h,v 1.9 2012/06/20 16:11:28 expcfi Exp $
    00007 //--------------------------------------------------------------------
    00008
    00009 #ifndef _ATTITUDEID_H
    00010 #define _ATTITUDEID_H
    00011
    00012 //--INCLUDE-----------------------------------------------------------
    00013 #include <vector>
    00014 #include <string>
    00015
    00016 #include "PointingData.h"
    00017 #include "CfiError.h"
    00018 #include "CfiId.h"
    00019 #include "TimeCorrelation.h"
    00020 #include "SatTransId.h"
    00021 #include "SatNomTransId.h"
    00022 #include "InstrTransId.h"
    00023 #include "SatId.h"
    00024 #include "ModelId.h"
    00025
    00026 //--NAMESPACES--------------------------------------------------------
    00027 using namespace std;
    00028
    00029 namespace EECFI
    00030 {
    00031
    00035   class Attitude: public CfiId
    00036   {
    00037     friend class Target;
    00038
    00039     public:
    00040
    00042       Attitude() throw (CfiError);
    00043
    00045       Attitude( const TimeCorrelation &timeId, const SatNomTransId &satNomTrId,
    00046                   const SatTransId &satTrId, const InstrTransId &instTrId ) throw (CfiError);
    00047
    00049       ~Attitude() throw (CfiError);
    00050
    00052       void setTransformations( const TimeCorrelation &timeId, const SatNomTransId &satNomTrId,
    00053                                const SatTransId &satTrId, const InstrTransId &instTrId) throw (CfiError);
    00054
    00056       void compute( const ModelId &modelId, const StateVector &stateVector,
    00057                     long targetFrame ) throw(CfiError);
    00058
    00060       void userSet( const ModelId &modelId, const StateVector &stateVector,
    00061                     long targetFrame, const double matrix[3][3],
    00062                     const double matrixRate[3][3], const double matrixRateRate[3][3],
    00063                     const double offset[3]) throw(CfiError);
    00064
    00066       AttitudeData getData() const throw (CfiError);
    00067
    00069       void setData( const AttitudeData &attitudeData ) throw (CfiError);
    00070
    00072       Coord changeFrame( const SatId &satId, const ModelId &modelId,
    00073                          long modeFlag, long frameFlagIn,
    00074                          long frameIdIn, long frameFlagOut, long frameIdOut,
    00075                          const StateVector &satStateVec, const Coord &statVecIn ) throw (CfiError);
    00077       Attitude const &operator=(Attitude const &att);
    00078
    00080       SatId satId() const;
    00081
    00082     protected:
    00083
    00085       GenericId* getId();  // this is the xo_orbit_id variable
    00086
    00088       long getCSEnum( long frame );
    00089
    00090     private:
    00091
    00092       TimeCorrelation timeId;
    00093       SatNomTransId   satNomTrId;
    00094       SatTransId      satTrId;
    00095       InstrTransId    instrTrId;
    00096   };
    00097
    00098 } // closing namespace
    00099
    00100 #endif