Earth Observation Mission CFI Software Orbit Software User Manual |
addInstance() | EECFI::CfiId | [protected] |
CfiClass() | EECFI::CfiClass | |
CfiId() | EECFI::CfiId | |
CfiId(const CfiId &cfiId) | 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 &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, 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(OrbitId &orbitIdIn) | EECFI::OrbitId | |
OrbitId() | EECFI::OrbitId | [protected] |
orbitInfoConfigure(long item, long option) const | EECFI::OrbitId | |
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) 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 | |
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 | |
status() const | EECFI::CfiId | |
subtractInstance() | EECFI::CfiId | [protected] |
throwWarn | EECFI::CfiClass | [protected] |
~CfiClass() EXCEPT | EECFI::CfiClass | |
~CfiId() NOEXCEPT | EECFI::CfiId | |
~OrbitId() EXCEPT | EECFI::OrbitId |