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Earth Observation Mission CFI Software Orbit Software User Manual for JAVA |
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Earth Observation Mission CFI Software Orbit Software User Manual for JAVA |
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| CfiClass() | EECFI.CfiClass | |
| CfiId() | EECFI.CfiId | |
| change(OrbitChangeData changeData) | EECFI.OrbitId | |
| check(OrbitFileDiagnosticsSettings settings) | EECFI.OrbitId | |
| close() | EECFI.OrbitId | |
| getAnx() | EECFI.OrbitId | |
| getGeoOrbitInfo() | EECFI.OrbitId | |
| getOrbitInfo(long absoluteOrbit) | EECFI.OrbitId | |
| getOrbitNumbersFromAbs(long absOrbit) | EECFI.OrbitId | |
| getOrbitNumbersFromPhase(long phase) | EECFI.OrbitId | |
| getOrbitNumbersFromRel(long relOrbit, long cycle) | EECFI.OrbitId | |
| getOsf() | EECFI.OrbitId | |
| getOsv() | EECFI.OrbitId | |
| getPrecisePropagConfig() | EECFI.OrbitId | |
| getValTime() | EECFI.OrbitId | |
| init(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, double time, long orbit0, long driftMode, double ascMlstDrift, double inclination, long irep, long icyc, double rlong, double ascMlst) | EECFI.OrbitId | |
| init(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, double time, long orbit0, final RefOrbitInfo refOrbitInfo) | EECFI.OrbitId | |
| init(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, double time, double[] pos, double[] vel, long absOrbit) | EECFI.OrbitId | |
| init(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, long orbitFileMode, final Vector< String > inputFiles, long timeInitMode, double time0, double time1, long orbit0, long orbit1) | EECFI.OrbitId | |
| init(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, double time, double[] pos, double[] vel, long absOrbit, final PropagPreciseConf preciseConf) | EECFI.OrbitId | |
| init(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, long orbitFileMode, final Vector< String > inputFiles, long timeInitMode, double time0, double time1, long orbit0, long orbit1, final PropagPreciseConf preciseConf) | EECFI.OrbitId | |
| init(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, final GeoOrbitInitData geoOrbitInit) | EECFI.OrbitId | |
| mode() | EECFI.CfiId | |
| OrbitId(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, double time, long orbit0, long driftMode, double ascMlstDrift, double inclination, long irep, long icyc, double rlong, double ascMlst) | EECFI.OrbitId | |
| OrbitId(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, double time, long orbit0, final RefOrbitInfo refOrbitInfo) | EECFI.OrbitId | |
| OrbitId(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, double time, double[] pos, double[] vel, long absOrbit) | EECFI.OrbitId | |
| OrbitId(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, long orbitFileMode, final Vector< String > inputFiles, long timeInitMode, double time0, double time1, long orbit0, long orbit1) | EECFI.OrbitId | |
| OrbitId(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, double time, double[] pos, double[] vel, long absOrbit, final PropagPreciseConf preciseConf) | EECFI.OrbitId | |
| OrbitId(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, long orbitFileMode, final Vector< String > inputFiles, long timeInitMode, double time0, double time1, long orbit0, long orbit1, final PropagPreciseConf preciseConf) | EECFI.OrbitId | |
| OrbitId(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, long orbitFileMode, OsfFileVector fileData, long timeInitMode, double time0, double time1, long orbit0, long orbit1) | EECFI.OrbitId | |
| OrbitId(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, long orbitFileMode, OrbitFileVector fileData, long timeInitMode, double time0, double time1, long orbit0, long orbit1) | EECFI.OrbitId | |
| OrbitId(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, long orbitFileMode, OrbitFileVector fileData, OrbitChangeData orbitChangeData, long timeInitMode, double time0, double time1, long orbit0, long orbit1) | EECFI.OrbitId | |
| OrbitId(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, long orbitFileMode, DorisFileVector fileData, long timeInitMode, double time0, double time1, long orbit0, long orbit1) | EECFI.OrbitId | |
| OrbitId(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, long orbitFileMode, DorisFileVector fileData, OrbitChangeData orbitChangeData, long timeInitMode, double time0, double time1, long orbit0, long orbit1) | EECFI.OrbitId | |
| OrbitId(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, long orbitFileMode, SP3FileVector fileData, long timeInitMode, double time0, double time1) | EECFI.OrbitId | |
| OrbitId(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, long orbitFileMode, OemFileVector fileData, long timeInitMode, double time0, double time1) | EECFI.OrbitId | |
| OrbitId(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, long orbitFileMode, TleFileVector fileData, long timeInitMode, double time0, double time1) | EECFI.OrbitId | |
| OrbitId(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, final GeoOrbitInitData geoOrbitInit) | EECFI.OrbitId | |
| orbitInfoConfigure(long item, long option) | EECFI.OrbitId | |
| osvCompute(long mode, long timeRef, double time) | EECFI.OrbitId | |
| osvComputeExtra(long extraChoice) | EECFI.OrbitId | |
| osvToTle(long timeMode, long timeRef, double time0, double time1, long orbit0, long orbit1) | EECFI.OrbitId | |
| positionOnOrbitToTime(long abs_orbit_number, long angle_type, double angle, double angle_rate, double angle_rate_rate, long deriv, long time_ref) | EECFI.OrbitId | |
| resetWarning() | EECFI.CfiClass | [static] |
| satId() | EECFI.OrbitId | |
| setAnx(final Vector< ANXExtra > anxList) | EECFI.OrbitId | |
| setGeoOrbitInfo(final GeoOrbitInfo geoOrbitInfo) | EECFI.OrbitId | |
| setOsf(final Vector< OsfRecords > osvRecList) | EECFI.OrbitId | |
| setOsv(final Vector< OsvRec > osvRecList) | EECFI.OrbitId | |
| setPrecisePropagConfig(final PropagPreciseConf preciseConf) | EECFI.OrbitId | |
| setValTime(final ValidityTime valTime) | EECFI.OrbitId | |
| setWarning() | EECFI.CfiClass | [static] |
| status() | EECFI.CfiId |
1.7.1