| DirectionCosMatrix1Axis(double _angle) | OrbitObserver | |
| DirectionCosMatrix2Axis(double _angle) | OrbitObserver | |
| DirectionCosMatrix3Axis(double _angle) | OrbitObserver | |
| ECEF2ECI(CAMdoubleVector _ECEFVector, double _jDay) | OrbitObserver | |
| ECEF2NEDVelocity(double _latitude, double _longitude, double _altitude, double _Vx, double _Vy, double _Vz) | OrbitObserver | |
| ECEF2WGS84(double _x, double _y, double _z, double _Vx, double _Vy, double _Vz) | OrbitObserver | |
| ECEFPosition2WGS84(double _x, double _y, double _z) | OrbitObserver | |
| ECI2COE(Vector ECI, Vector VECI, Keplerian &myCOE, double &a, double &e, double &i, double &Lon, double &Arg, double &tru) | OrbitObserver | |
| ECI2ECEF(CAMdoubleVector _ECIVector, double _jDay) | OrbitObserver | |
| Initialize()=0 | OrbitObserver | [pure virtual] |
| lat_lon(double latlon, char sector) | OrbitObserver | |
| NED2ECEFVelocity(double _latitude, double _longitude, double _altitude, double _velocityNorth, double _velocityEast, double _velocityDown) | OrbitObserver | |
| OrbitObserver() | OrbitObserver | |
| Run()=0 | OrbitObserver | [pure virtual] |
| TangentPlaneState(AshtechG12_GPS_PhysicalDevice::Position recPos, CAMdoubleVector &_WGS84Vector) | OrbitObserver | |
| WGS2ECEFPosition(double _latitude, double _longitude, double _altitude) | OrbitObserver | |
| WGS842ECEF(double _latitude, double _longitude, double _altitude, double _velocityNorth, double _velocityEast, double _velocityDown) | OrbitObserver | |
| ~OrbitObserver() | OrbitObserver | [virtual] |
