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Earth Observation Mission CFI Software Pointing Software User Manual for JAVA |
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| 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 |
1.7.1