Earth Observation Mission CFI Software Lib Software User Manual for JAVA |
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. |
Attitude frame coordinate systems.
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.