Earth Observation Mission CFI Software Pointing Software User Manual for JAVA |
CfiClass() | EECFI.CfiClass | |
CfiId() | EECFI.CfiId | |
CfiId(CfiId cfiId) | EECFI.CfiId | |
eq(CfiId cfiId) | EECFI.CfiId | |
getAngles() | EECFI.SatTransId | |
getFile() | EECFI.SatTransId | |
getHarmonic() | EECFI.SatTransId | |
getMatrix() | EECFI.SatTransId | |
getQuatPlusAngles() | EECFI.SatTransId | |
getQuatPlusMatrix() | EECFI.SatTransId | |
init(double[] angle) | EECFI.SatTransId | |
init(double[][] matrix) | EECFI.SatTransId | |
init(long angleType, final Vector< Long > harmTypePitch, final Vector< Long > harmTypeRoll, final Vector< Long > harmTypeYaw, final Vector< Double > harmCoeffPitch, final Vector< Double > harmCoeffRoll, final Vector< Double > harmCoeffYaw) | EECFI.SatTransId | |
init(long inertialFrame, final Vector< AttRec > quaternions, double[][] matrix) | EECFI.SatTransId | |
init(long inertialFrame, final Vector< AttRec > quaternions, double[] angles) | EECFI.SatTransId | |
init(final TimeCorrelation timeId, final Vector< String > files, String auxiliaryFile, long timeInitMode, long timeRef, double time0, double time1) | EECFI.SatTransId | |
mode() | EECFI.CfiId | |
resetWarning() | EECFI.CfiClass | |
satId() | EECFI.SatTransId | |
SatTransId() | EECFI.SatTransId | |
setAngles(final AngleModel angleModel) | EECFI.SatTransId | |
setAzElDefinition(final AzElDefinition azElDef) | EECFI.SatTransId | |
setFile(final SatAttFileModel fileModel) | EECFI.SatTransId | |
setHarmonic(final HarmonicModel harmModel) | EECFI.SatTransId | |
setMatrix(final MatrixModel matrixModel) | EECFI.SatTransId | |
setQuatPlusAngles(final QuatPlusAnglesModel quatPlusAnglesModel) | EECFI.SatTransId | |
setQuatPlusMatrix(final QuatPlusMatrixModel quatPlusMatrixModel) | EECFI.SatTransId | |
setWarning() | EECFI.CfiClass | |
status() | EECFI.CfiId |