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 | |
GetState(ClientSocket *_clientSocket, int _vehicleID, double _currentTime, CAMdoubleVector _acceleration, double _newMass) | OrbitPropObserver | |
Initialize() | OrbitPropObserver | [virtual] |
lat_lon(double latlon, char sector) | OrbitObserver | |
m_acceleration | OrbitPropObserver | [private] |
m_clientSocket | OrbitPropObserver | [private] |
m_currentTime | OrbitPropObserver | [private] |
m_ECIVector | OrbitPropObserver | [private] |
m_InitialTime | OrbitPropObserver | [private] |
m_mass | OrbitPropObserver | [private] |
m_SpaceVehicleMeanCOE | OrbitPropObserver | [private] |
m_SpaceVehicleOsculatingCOE | OrbitPropObserver | [private] |
m_vehicleID | OrbitPropObserver | [private] |
m_whorl | OrbitPropObserver | [private] |
NED2ECEFVelocity(double _latitude, double _longitude, double _altitude, double _velocityNorth, double _velocityEast, double _velocityDown) | OrbitObserver | |
OrbitObserver() | OrbitObserver | |
OrbitPropObserver() | OrbitPropObserver | |
OrbitPropObserver(TiXmlHandle handle, Whorl *ptr_whorl) | OrbitPropObserver | |
Parse(TiXmlHandle handle) | OrbitPropObserver | |
ParseState(string _reply) | OrbitPropObserver | |
Run() | OrbitPropObserver | [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] |
~OrbitPropObserver() | OrbitPropObserver | [virtual] |