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