| Earth Observation Mission CFI Software Lib Software User Manual for JAVA |

Variables

# CoordinateSystemEnum

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_PEF = 8
| Earth Fixed coordinate system.
static long | EECFI::EnumLib.XLCFI_CS_EF = 9
| Earth Fixed coordinate system.
static long | EECFI::EnumLib.XLCFI_CS_TOPOCENTRIC = 10
| Topocentric coordinate system .
static long | EECFI::EnumLib.XLCFI_CS_SAT_ORBITAL_REF = 11
| Orbital frame.
static long | EECFI::EnumLib.XLCFI_CS_SAT_NOMINAL_ATT = 12
| Satellite nominal attitude frame.
static long | EECFI::EnumLib.XLCFI_CS_SAT_ATT = 13
| Satellite attitude frame.
static long | EECFI::EnumLib.XLCFI_CS_INSTR_ATT = 14
| Instrument attitude frame.

## Detailed Description

Coordinate Systems.

## Variable Documentation

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 = 9`[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 = 14`[static, inherited]`

Instrument attitude frame.

long EECFI.EnumLib.XLCFI_CS_MOD = 6`[static, inherited]`

Mean of Date coordinate system .

long EECFI.EnumLib.XLCFI_CS_PEF = 8`[static, inherited]`

Earth Fixed coordinate system.

long EECFI.EnumLib.XLCFI_CS_SAT_ATT = 13`[static, inherited]`

Satellite attitude frame.

long EECFI.EnumLib.XLCFI_CS_SAT_NOMINAL_ATT = 12`[static, inherited]`

Satellite nominal attitude frame.

long EECFI.EnumLib.XLCFI_CS_SAT_ORBITAL_REF = 11`[static, inherited]`

Orbital frame.

long EECFI.EnumLib.XLCFI_CS_TOD = 7`[static, inherited]`

True of Date coordinate system.

long EECFI.EnumLib.XLCFI_CS_TOPOCENTRIC = 10`[static, inherited]`

Topocentric coordinate system .

long EECFI.EnumLib.XLCFI_CS_UNDEF = 0`[static, inherited]`

Undefined.