DEIMOS
Earth Observation Mission CFI Software
Lib Software User Manual
for JAVA
ESA

XLAttitudeFrameEnum

Attitude frame coordinate systems. More...

Variables

static final long EECFI::EnumLib.XLCFI_CS_SAT_ORBITAL_REF = 0
 Orbital frame.
static final long EECFI::EnumLib.XLCFI_CS_SAT_NOMINAL_ATT = 1
 Satellite nominal attitude frame.
static final long EECFI::EnumLib.XLCFI_CS_SAT_ATT = 2
 Satellite attitude frame.
static final long EECFI::EnumLib.XLCFI_CS_INSTR_ATT = 3
 Instrument attitude frame.

Detailed Description

Attitude frame coordinate systems.


Variable Documentation

final long EECFI.EnumLib.XLCFI_CS_INSTR_ATT = 3 [static, inherited]

Instrument attitude frame.

final long EECFI.EnumLib.XLCFI_CS_SAT_ATT = 2 [static, inherited]

Satellite attitude frame.

final long EECFI.EnumLib.XLCFI_CS_SAT_NOMINAL_ATT = 1 [static, inherited]

Satellite nominal attitude frame.

final long EECFI.EnumLib.XLCFI_CS_SAT_ORBITAL_REF = 0 [static, inherited]

Orbital frame.


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