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Earth Observation Mission CFI Software DataHandling Software User Manual for JAVA |
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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).
1.7.1