DEIMOS
Earth Observation Mission CFI Software
Pointing Software User Manual
ESA

EECFI::Target Member List

This is the complete list of members for EECFI::Target, including all inherited members.
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
numLosTargetEECFI::Target
numUserTargetEECFI::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
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
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
throwWarnEECFI::CfiClass [protected]
~CfiClass()EECFI::CfiClass
~CfiId()EECFI::CfiId
~Target()EECFI::Target

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