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Earth Observation Mission CFI Software Orbit Software User Manual |
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Earth Observation Mission CFI Software Orbit Software User Manual |
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| addInstance() | EECFI::CfiId | [protected] |
| CfiId() | EECFI::CfiId | |
| CfiId(const CfiId &other) | EECFI::CfiId | |
| change(const OrbitChangeData &changeData) | EECFI::OrbitId | |
| check(const OrbitFileDiagnosticsSettings &settings) const | EECFI::OrbitId | |
| getAnx() const | EECFI::OrbitId | |
| getGeoOrbitInfo() | EECFI::OrbitId | |
| getOrbitInfo(long absoluteOrbit) const | EECFI::OrbitId | |
| getOrbitNumbersFromAbs(long absOrbit) const | EECFI::OrbitId | |
| getOrbitNumbersFromPhase(long phase) const | EECFI::OrbitId | |
| getOrbitNumbersFromRel(long relOrbit, long cycle) const | EECFI::OrbitId | |
| getOsf() const | EECFI::OrbitId | |
| getOsv() const | EECFI::OrbitId | |
| getPrecisePropagConfig() const | EECFI::OrbitId | |
| getValTime() const | EECFI::OrbitId | |
| init(const SatId &satId, const ModelId &modelId, const 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(const SatId &satId, const ModelId &modelId, const TimeCorrelation &timeCor, long timeRef, double time, long orbit0, const RefOrbitInfo &refOrbitInfo) | EECFI::OrbitId | |
| init(const SatId &satId, const ModelId &modelId, const TimeCorrelation &timeCor, long timeRef, double time, const double pos[3], const double vel[3], long absOrbit) | EECFI::OrbitId | |
| init(const SatId &satId, const ModelId &modelId, const TimeCorrelation &timeCor, long timeRef, long orbitFileMode, const std::vector< std::string > &inputFiles, long timeInitMode, double time0, double time1, long orbit0, long orbit1) | EECFI::OrbitId | |
| init(const SatId &satId, const ModelId &modelId, const TimeCorrelation &timeCor, long timeRef, double time, const double pos[3], const double vel[3], long absOrbit, const PropagPreciseConf &preciseConf) | EECFI::OrbitId | |
| init(const SatId &satId, const ModelId &modelId, const TimeCorrelation &timeCor, long timeRef, long orbitFileMode, const std::vector< std::string > &inputFiles, long timeInitMode, double time0, double time1, long orbit0, long orbit1, const PropagPreciseConf &preciseConf) | EECFI::OrbitId | |
| init(const SatId &satId, const ModelId &modelId, const TimeCorrelation &timeCor, const GeoOrbitInitData &geoOrbitInit) | EECFI::OrbitId | |
| mode() const | EECFI::CfiId | |
| operator=(const OrbitId &other) | EECFI::OrbitId | |
| EECFI::CfiId::operator=(CfiId const &cfiId) | EECFI::CfiId | |
| OrbitId(const OrbitId &other) | EECFI::OrbitId | |
| OrbitId(const SatId &satId, const ModelId &modelId, const 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(const SatId &satId, const ModelId &modelId, const TimeCorrelation &timeCor, long timeRef, double time, long orbit0, const RefOrbitInfo &refOrbitInfo) | EECFI::OrbitId | |
| OrbitId(const SatId &satId, const ModelId &modelId, const TimeCorrelation &timeCor, long timeRef, double time, const double pos[3], const double vel[3], long absOrbit) | EECFI::OrbitId | |
| OrbitId(const SatId &satId, const ModelId &modelId, const TimeCorrelation &timeCor, long timeRef, long orbitFileMode, const std::vector< std::string > &inputFiles, long timeInitMode, double time0, double time1, long orbit0, long orbit1) | EECFI::OrbitId | |
| OrbitId(const SatId &satId, const ModelId &modelId, const TimeCorrelation &timeCor, long timeRef, double time, const double pos[3], const double vel[3], long absOrbit, const PropagPreciseConf &preciseConf) | EECFI::OrbitId | |
| OrbitId(const SatId &satId, const ModelId &modelId, const TimeCorrelation &timeCor, long timeRef, long orbitFileMode, const std::vector< std::string > &inputFiles, long timeInitMode, double time0, double time1, long orbit0, long orbit1, const PropagPreciseConf &preciseConf) | EECFI::OrbitId | |
| OrbitId(const SatId &satId, const ModelId &modelId, const TimeCorrelation &timeCor, long timeRef, long orbitFileMode, const std::vector< OsfFile > &osfData, long timeInitMode, double time0, double time1, long orbit0, long orbit1) | EECFI::OrbitId | |
| OrbitId(const SatId &satId, const ModelId &modelId, const TimeCorrelation &timeCor, long timeRef, long orbitFileMode, const std::vector< OrbitFile > &osvData, long timeInitMode, double time0, double time1, long orbit0, long orbit1) | EECFI::OrbitId | |
| OrbitId(const SatId &satId, const ModelId &modelId, const TimeCorrelation &timeCor, long timeRef, long orbitFileMode, const std::vector< OrbitFile > &osvData, const OrbitChangeData &orbitChangeData, long timeInitMode, double time0, double time1, long orbit0, long orbit1) | EECFI::OrbitId | |
| OrbitId(const SatId &satId, const ModelId &modelId, const TimeCorrelation &timeCor, long timeRef, long orbitFileMode, const std::vector< DorisFile > &dorisData, long timeInitMode, double time0, double time1, long orbit0, long orbit1) | EECFI::OrbitId | |
| OrbitId(const SatId &satId, const ModelId &modelId, const TimeCorrelation &timeCor, long timeRef, long orbitFileMode, const std::vector< DorisFile > &dorisData, const OrbitChangeData &orbitChangeData, long timeInitMode, double time0, double time1, long orbit0, long orbit1) | EECFI::OrbitId | |
| OrbitId(const SatId &satId, const ModelId &modelId, const TimeCorrelation &timeCor, long timeRef, long orbitFileMode, const std::vector< SP3File > &sp3Data, long timeInitMode, double time0, double time1) | EECFI::OrbitId | |
| OrbitId(const SatId &satId, const ModelId &modelId, const TimeCorrelation &timeCor, const GeoOrbitInitData &geoOrbitInit) | EECFI::OrbitId | |
| OrbitId(const SatId &satId, const ModelId &modelId, const TimeCorrelation &timeCor, long timeRef, long orbitFileMode, const std::vector< OemFile > &oemData, long timeInitMode, double time0, double time1) | EECFI::OrbitId | |
| OrbitId(const SatId &satId, const ModelId &modelId, const TimeCorrelation &timeCor, long timeRef, long orbitFileMode, const std::vector< TleFile > &tleData, long timeInitMode, double time0, double time1) | EECFI::OrbitId | |
| OrbitId(OrbitId &orbitIdIn) | EECFI::OrbitId | |
| OrbitId() | EECFI::OrbitId | [protected] |
| orbitInfoConfigure(long item, long option) const | EECFI::OrbitId | |
| osvCompute(long mode, long timeRef, double time) | EECFI::OrbitId | |
| osvComputeExtra(long extraChoice) const | EECFI::OrbitId | |
| osvToTle(long timeMode, long timeRef, double time0, double time1, long orbit0, long orbit1) const | EECFI::OrbitId | |
| positionOnOrbitToTime(long abs_orbit_number, long angle_type, double angle, double angle_rate, double angle_rate_rate, long deriv, long time_ref) const | EECFI::OrbitId | |
| resetWarning() | EECFI::CfiClass | [static] |
| satId() const | EECFI::OrbitId | |
| setAnx(const std::vector< ANXExtra > &anxList) | EECFI::OrbitId | |
| setGeoOrbitInfo(const GeoOrbitInfo &geoOrbitInfo) | EECFI::OrbitId | |
| setOsf(const std::vector< OsfRecords > &osvRecList) | EECFI::OrbitId | |
| setOsv(const std::vector< OsvRec > &osvRecList) | EECFI::OrbitId | |
| setPrecisePropagConfig(const PropagPreciseConf &preciseConf) | EECFI::OrbitId | |
| setValTime(const ValidityTime &valTime) | EECFI::OrbitId | |
| setWarning() | EECFI::CfiClass | [static] |
| status() const | EECFI::CfiId | |
| subtractInstance() | EECFI::CfiId | [protected] |
| throwWarn | EECFI::CfiClass | [protected, static] |
| ~CfiId() EXCEPT | EECFI::CfiId | [virtual] |
| ~OrbitId() EXCEPT | EECFI::OrbitId | [virtual] |
1.7.1