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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] |
| CfiClass() | EECFI::CfiClass | |
| CfiId() | EECFI::CfiId | |
| CfiId(const CfiId &cfiId) | EECFI::CfiId | |
| 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, double pos[3], double vel[3], long absOrbit) | EECFI::OrbitId | |
| init(const SatId &satId, const ModelId &modelId, const TimeCorrelation &timeCor, long timeRef, long orbitFileMode, const vector< 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, double pos[3], 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 vector< 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() | EECFI::CfiId | |
| operator=(const OrbitId &orbitIdIn) | EECFI::OrbitId | |
| EECFI::CfiId::operator=(CfiId const &cfiId) | EECFI::CfiId | |
| 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, double pos[3], double vel[3], long absOrbit) | EECFI::OrbitId | |
| OrbitId(const SatId &satId, const ModelId &modelId, const TimeCorrelation &timeCor, long timeRef, long orbitFileMode, const vector< 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, double pos[3], 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 vector< 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, 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, 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, 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, const GeoOrbitInitData &geoOrbitInit) | EECFI::OrbitId | |
| OrbitId(OrbitId &orbitIdIn) | EECFI::OrbitId | |
| OrbitId() | EECFI::OrbitId | [protected] |
| osvCompute(long mode, long timeRef, double time) const | EECFI::OrbitId | |
| osvComputeExtra(long extraChoice) const | 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) const | EECFI::OrbitId | |
| resetWarning() | EECFI::CfiClass | |
| satId() const | EECFI::OrbitId | |
| setAnx(const vector< ANXExtra > &anxList) | EECFI::OrbitId | |
| setGeoOrbitInfo(const GeoOrbitInfo &geoOrbitInfo) | EECFI::OrbitId | |
| setOsf(const vector< OsfRecords > &osvRecList) | EECFI::OrbitId | |
| setOsv(const vector< OsvRec > &osvRecList) | EECFI::OrbitId | |
| setPrecisePropagConfig(const PropagPreciseConf &preciseConf) | EECFI::OrbitId | |
| setValTime(const ValidityTime &valTime) | EECFI::OrbitId | |
| setWarning() | EECFI::CfiClass | |
| status() | EECFI::CfiId | |
| subtractInstance() | EECFI::CfiId | [protected] |
| throwWarn | EECFI::CfiClass | [protected] |
| ~CfiClass() | EECFI::CfiClass | |
| ~CfiId() | EECFI::CfiId | |
| ~OrbitId() | EECFI::OrbitId |
1.7.1