gSatWrapper.hpp   gSatWrapper.hpp 
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#include "gsatellite/gSatTEME.hpp" #include "gsatellite/gSatTEME.hpp"
#include "gsatellite/gTime.hpp" #include "gsatellite/gTime.hpp"
//constants for predict visibility //constants for predict visibility
#define RADAR_SUN 1 #define RADAR_SUN 1
#define VISIBLE 2 #define VISIBLE 2
#define RADAR_NIGHT 3 #define RADAR_NIGHT 3
#define NOT_VISIBLE 4 #define NOT_VISIBLE 4
//! Wrapper allowing compatibility between gsat and Stellarium/Qt. //! Wrapper allowing compatibility between gsat and Stellarium/Qt.
//! @ingroup satellites
class gSatWrapper class gSatWrapper
{ {
public: public:
gSatWrapper(QString designation, QString tle1,QString tle2); gSatWrapper(QString designation, QString tle1,QString tle2);
~gSatWrapper(); ~gSatWrapper();
// Operation updateEpoch // Operation updateEpoch
//! @brief This operation update Epoch timestamp for gSatTEME object //! @brief This operation update Epoch timestamp for gSatTEME object
//! from Stellarium Julian Date. //! from Stellarium Julian Date.
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//! 1 if RADAR_SUN //! 1 if RADAR_SUN
//! 2 if VISIBLE //! 2 if VISIBLE
//! 3 if RADAR_NIGHt //! 3 if RADAR_NIGHt
//! 3 if NOT_VISIBLE //! 3 if NOT_VISIBLE
//! @par References //! @par References
//! Fundamentals of Astrodynamis and Applications (Third Edition) pg 898 //! Fundamentals of Astrodynamis and Applications (Third Edition) pg 898
//! David A. Vallado //! David A. Vallado
int getVisibilityPredict(); int getVisibilityPredict();
double getPhaseAngle(); double getPhaseAngle();
gTime getEpoch() { return epoch; }
private: //private:
// Operation calcObserverECIPosition // Operation calcObserverECIPosition
//! @brief This operation compute the observer ECI coordinates in G eocentric //! @brief This operation compute the observer ECI coordinates in G eocentric
//! Ecuatorial Coordinate System (IJK) for the ai_epoch time. //! Ecuatorial Coordinate System (IJK) for the ai_epoch time.
//! This position can be asumed as observer position in TEME framew ork without an appreciable error. //! This position can be asumed as observer position in TEME framew ork without an appreciable error.
//! ECI axis (IJK) are parallel to StelCore::EquinoxEQ Framework bu t centered in the earth centre //! ECI axis (IJK) are parallel to StelCore::EquinoxEQ Framework bu t centered in the earth centre
//! instead the observer position. //! instead the observer position.
//! @par References //! @par References
//! Orbital Coordinate Systems, Part II //! Orbital Coordinate Systems, Part II
//! Dr. T.S. Kelso //! Dr. T.S. Kelso
//! http://www.celestrak.com/columns/v02n02/ //! http://www.celestrak.com/columns/v02n02/
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