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 | |||

skipping to change at line 112 | skipping to change at line 117 | |||

//! @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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