 |
Earth Observation Mission CFI Software Lib Software User Manual for JAVA |
 |
| |
Earth Observation Mission CFI Software Lib Software User Manual for JAVA |
|
Coordinate Systems. More...
Variables | |
| static long | EECFI::EnumLib.XLCFI_CS_UNDEF = 0 |
| Undefined. | |
| static long | EECFI::EnumLib.XLCFI_CS_GALACTIC = 1 |
| Galactic coordinate system. | |
| static long | EECFI::EnumLib.XLCFI_CS_BM1950 = 2 |
| Barycentric Mean of 2000.0 coordinate system. | |
| static long | EECFI::EnumLib.XLCFI_CS_BM2000 = 3 |
| Barycentric Mean of 2000.0 coordinate system. | |
| static long | EECFI::EnumLib.XLCFI_CS_HM2000 = 4 |
| Heliocentric Mean of 2000.0 coordinate system. | |
| static long | EECFI::EnumLib.XLCFI_CS_GM2000 = 5 |
| Geocentric Mean of 2000.0 coordinate system. | |
| static long | EECFI::EnumLib.XLCFI_CS_MOD = 6 |
| Mean of Date coordinate system . | |
| static long | EECFI::EnumLib.XLCFI_CS_TOD = 7 |
| True of Date coordinate system. | |
| static long | EECFI::EnumLib.XLCFI_CS_EF = 8 |
| Earth Fixed coordinate system. | |
| static long | EECFI::EnumLib.XLCFI_CS_TOPOCENTRIC = 9 |
| Topocentric coordinate system . | |
| static long | EECFI::EnumLib.XLCFI_CS_SAT_ORBITAL_REF = 10 |
| Orbital frame. | |
| static long | EECFI::EnumLib.XLCFI_CS_SAT_NOMINAL_ATT = 11 |
| Satellite nominal attitude frame. | |
| static long | EECFI::EnumLib.XLCFI_CS_SAT_ATT = 12 |
| Satellite attitude frame. | |
| static long | EECFI::EnumLib.XLCFI_CS_INSTR_ATT = 13 |
| Instrument attitude frame. | |
Coordinate Systems.
long EECFI.EnumLib.XLCFI_CS_BM1950 = 2 [static, inherited] |
Barycentric Mean of 2000.0 coordinate system.
long EECFI.EnumLib.XLCFI_CS_BM2000 = 3 [static, inherited] |
Barycentric Mean of 2000.0 coordinate system.
long EECFI.EnumLib.XLCFI_CS_EF = 8 [static, inherited] |
Earth Fixed coordinate system.
long EECFI.EnumLib.XLCFI_CS_GALACTIC = 1 [static, inherited] |
Galactic coordinate system.
long EECFI.EnumLib.XLCFI_CS_GM2000 = 5 [static, inherited] |
Geocentric Mean of 2000.0 coordinate system.
long EECFI.EnumLib.XLCFI_CS_HM2000 = 4 [static, inherited] |
Heliocentric Mean of 2000.0 coordinate system.
long EECFI.EnumLib.XLCFI_CS_INSTR_ATT = 13 [static, inherited] |
Instrument attitude frame.
long EECFI.EnumLib.XLCFI_CS_MOD = 6 [static, inherited] |
Mean of Date coordinate system .
long EECFI.EnumLib.XLCFI_CS_SAT_ATT = 12 [static, inherited] |
Satellite attitude frame.
long EECFI.EnumLib.XLCFI_CS_SAT_NOMINAL_ATT = 11 [static, inherited] |
Satellite nominal attitude frame.
long EECFI.EnumLib.XLCFI_CS_SAT_ORBITAL_REF = 10 [static, inherited] |
Orbital frame.
long EECFI.EnumLib.XLCFI_CS_TOD = 7 [static, inherited] |
True of Date coordinate system.
long EECFI.EnumLib.XLCFI_CS_TOPOCENTRIC = 9 [static, inherited] |
Topocentric coordinate system .
long EECFI.EnumLib.XLCFI_CS_UNDEF = 0 [static, inherited] |
Undefined.
1.7.1