gSatWrapper.hpp   gSatWrapper.hpp 
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//! from Stellarium Julian Date. //! from Stellarium Julian Date.
void updateEpoch(); void updateEpoch();
void setEpoch(double ai_julianDaysEpoch); void setEpoch(double ai_julianDaysEpoch);
// Operation getTEMEPos // Operation getTEMEPos
//! @brief This operation isolate gSatTEME getPos operation. //! @brief This operation isolate gSatTEME getPos operation.
//! @return Vec3d with TEME position. Units measured in Km. //! @return Vec3d with TEME position. Units measured in Km.
Vec3d getTEMEPos(); Vec3d getTEMEPos();
// Operation getSunECIPos
//! @brief Get Sun positions in ECI system.
//! @return Vec3d with ECI position.
Vec3d getSunECIPos();
// Operation getTEMEVel // Operation getTEMEVel
//! @brief This operation isolate gSatTEME getVel operation. //! @brief This operation isolate gSatTEME getVel operation.
//! @return Vec3d with TEME speed. Units measured in Km/s. //! @return Vec3d with TEME speed. Units measured in Km/s.
Vec3d getTEMEVel(); Vec3d getTEMEVel();
// Operation: getSubPoint // Operation: getSubPoint
//! @brief This operation isolate getSubPoint method of gSatTEME obj ect. //! @brief This operation isolate getSubPoint method of gSatTEME obj ect.
//! @return Vec3d Geographical coordinates\n //! @return Vec3d Geographical coordinates\n
//! Latitude: Coord[0] measured in degrees\n //! Latitude: Coord[0] measured in degrees\n
//! Longitude: Coord[1] measured in degrees\n //! Longitude: Coord[1] measured in degrees\n
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//! @return //! @return
//! 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();
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
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