| Earth Observation Mission CFI Software Orbit Software User Manual |

# EECFI::OrbitId Member List

This is the complete list of members for EECFI::OrbitId, including all inherited members.

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 |