Earth Observation Mission CFI Software DataHandling Software User Manual for JAVA |
Class for containing satellite state vector for a given time. More...
Public Member Functions | |
OsvRec () | |
Constructor. | |
OsvRec (final double taiTim, final double utcTim, final double ut1Tim, final long absOrbi, final long referFrame, final long timeRef, double[] posi, double[] velo, final double qual) | |
Constructor with parameters. | |
Public Attributes | |
double | taiTime |
TAI time. | |
double | utcTime |
UTC time. | |
double | ut1Time |
UT1 time. | |
long | absOrbit |
Absolute orbit. | |
long | refFrame |
Reference frame. | |
long | timeRefOf |
Reference time. | |
double[] | position |
Position vector (x, y, z components). | |
double[] | velocity |
Velocity vector (x, y, z components). | |
double | quality |
Quality index. |
Class for containing satellite state vector for a given time.
EECFI.OsvRec.OsvRec | ( | ) |
Constructor.
EECFI.OsvRec.OsvRec | ( | final double | taiTim, | |
final double | utcTim, | |||
final double | ut1Tim, | |||
final long | absOrbi, | |||
final long | referFrame, | |||
final long | timeRef, | |||
double[] | posi, | |||
double[] | velo, | |||
final double | qual | |||
) |
Constructor with parameters.
Absolute orbit.
double [] EECFI.OsvRec.position |
Position vector (x, y, z components).
double EECFI.OsvRec.quality |
Quality index.
Reference frame.
double EECFI.OsvRec.taiTime |
TAI time.
Reference time.
double EECFI.OsvRec.ut1Time |
UT1 time.
double EECFI.OsvRec.utcTime |
UTC time.
double [] EECFI.OsvRec.velocity |
Velocity vector (x, y, z components).