|
Earth Observation Mission CFI Software Pointing Software User Manual |
|
| addInstance() | EECFI::CfiId | [protected] |
| CfiClass() | EECFI::CfiClass | |
| CfiId() | EECFI::CfiId | |
| CfiId(const CfiId &cfiId) | EECFI::CfiId | |
| extraAux(long choice, long targetType, long targetNumber, vector< double > &extraResult, vector< double > &extraResultRate, vector< double > &extraResultRateRate) | EECFI::Target | |
| extraEfTarget(long choice, long targetType, long targetNumber, double freq, vector< double > &efResultRate, vector< double > &efResultRateRate) | EECFI::Target | |
| extraMain(long choice, long targetType, long targetNumber, vector< double > &mainResult, vector< double > &mainResultRate, vector< double > &mainResultRateRate) | EECFI::Target | |
| extraSpecularReflection(long choice, long targetType, long targetNumber, double deflectionNorth, double deflectionEast, vector< double > &specRefResult, vector< double > &specRefResultRate, vector< double > &specRefResultRateRate) | EECFI::Target | |
| extraTargetToMoon(long choice, long targetType, long targetNumber, long iray, double freq, vector< double > &moonResult, vector< double > &moonResultRate, vector< double > &moonResultRateRate) | EECFI::Target | |
| extraTargetToSun(long choice, long targetType, long targetNumber, long iray, double freq, vector< double > &sunResult, vector< double > &sunResultRate, vector< double > &sunResultRateRate) | EECFI::Target | |
| extraVector(long choice, long targetType, long targetNumber, vector< double > &vectorResult, vector< double > &vectorResultRate, vector< double > &vectorResultRateRate) | EECFI::Target | |
| getData() const | EECFI::Target | |
| getId() | EECFI::Target | [protected] |
| mode() | EECFI::CfiId | |
| multiTargetInter(const SatId &satId, long deriv, long interFlag, double losAz, double losEl, long numTarget, vector< double > &geodAlt, double losAzRate, double losElRate, long iray, double freq) | EECFI::Target | |
| multiTargetTravelTime(const SatId &satId, long deriv, double losAz, double losEl, long numTarget, vector< double > &travelTime, double losAzRate, double losElRate, double travelTimeRate, long iray, double freq) | EECFI::Target | |
| numLosTarget | EECFI::Target | |
| numUserTarget | EECFI::Target | |
| operator=(Target const &target) | EECFI::Target | |
| EECFI::CfiId::operator=(CfiId const &cfiId) | EECFI::CfiId | |
| resetWarning() | EECFI::CfiClass | |
| satId() const | EECFI::Target | |
| setWarning() | EECFI::CfiClass | |
| status() | EECFI::CfiId | |
| subtractInstance() | EECFI::CfiId | [protected] |
| Target(const Attitude &attitude, const DemId &demId, const AtmosId &atmosId) | EECFI::Target | |
| targetAltitude(const SatId &satId, long deriv, double losAz, double geodAlt, double losAzRate, long iray, double freq) | EECFI::Target | |
| targetDRS(const SatId &satId, long deriv, double drsPos[3], double drsVel[3]) | EECFI::Target | |
| targetGeneric(const SatId &satId, long deriv, double targPos[3], double targVel[3], double targAcc[3]) | EECFI::Target | |
| targetGroundRange(const SatId &satId, long deriv, double losAz, double losEl, double geodAlt, double distance, double losAzRate, double losElRate) | EECFI::Target | |
| targetIncidenceAngle(const SatId &satId, long deriv, double losAz, double incidenceAngle, double geodAlt, double losAzRate) | EECFI::Target | |
| targetInter(const SatId &satId, long deriv, long interFlag, double losAz, double losEl, double geodAlt, double losAzRate, double losElRate, long iray, double freq) | EECFI::Target | |
| targetListInter(const SatId &satId, long deriv, long interFlag, const InstrumentData &instrData, double geodAlt, TargetOutput &targOut) | EECFI::Target | |
| targetRange(const SatId &satId, long deriv, double losAz, double range, double geodAlt, double losAzRate, double rangeRate) | EECFI::Target | |
| targetRangeRate(const SatId &satId, long deriv, double efRangeRate, double range, double geodAlt, double efRangeRateRate, double rangeRate) | EECFI::Target | |
| targetReflected(const SatId &satId, long deriv, double geodAlt, double deflectionNorth, double deflectionEast, long sourceType, vector< double > &sourceParam) | EECFI::Target | |
| targetSc(const SatId &satId1, const SatId &satId2, const Attitude &att2, long deriv) | EECFI::Target | |
| targetStar(const SatId &satId, long deriv, double starRa, double starDec, double starRaRate, double starDecRate, long iray, double freq) | EECFI::Target | |
| targetStation(const SatId &satId, long deriv, double geocLong, double geodLat, double geodAlt, double minLinkEl) | EECFI::Target | |
| targetTangent(const SatId &satId, long deriv, double losAz, double losEl, double losAzRate, double losElRate, long iray, double freq) | EECFI::Target | |
| targetTangentMoon(const SatId &satId, long deriv, long iray, double freq) | EECFI::Target | |
| targetTangentSun(const SatId &satId, long deriv, long iray, double freq) | EECFI::Target | |
| targetTravelTime(const SatId &satId, long deriv, double losAz, double losEl, double travelTime, double losAzRate, double losElRate, double travelTimeRate, long iray, double freq) | EECFI::Target | |
| throwWarn | EECFI::CfiClass | [protected] |
| ~CfiClass() | EECFI::CfiClass | |
| ~CfiId() | EECFI::CfiId | |
| ~Target() | EECFI::Target |
1.7.1