Earth Observation Mission CFI Software Pointing Software User Manual |
addInstance() | EECFI::CfiId | [protected] |
Attitude() | EECFI::Attitude | |
Attitude(const TimeCorrelation &timeId, const SatNomTransId &satNomTrId, const SatTransId &satTrId, const InstrTransId &instTrId) | EECFI::Attitude | |
CfiClass() | EECFI::CfiClass | |
CfiId() | EECFI::CfiId | |
CfiId(const CfiId &cfiId) | EECFI::CfiId | |
changeFrame(const SatId &satId, const ModelId &modelId, long modeFlag, long frameFlagIn, long frameIdIn, long frameFlagOut, long frameIdOut, const StateVector &satStateVec, const Coord &statVecIn) | EECFI::Attitude | |
compute(const ModelId &modelId, const StateVector &stateVector, long targetFrame) | EECFI::Attitude | |
eraseObject() | EECFI::Attitude | [protected] |
getAttitudeData(long dataType, long sourceRefType, long sourceRef) const | EECFI::Attitude | |
getData() const | EECFI::Attitude | |
getId() const | EECFI::Attitude | [protected] |
mode() const | EECFI::CfiId | |
operator=(Attitude const &att) | EECFI::Attitude | |
EECFI::CfiId::operator=(CfiId const &cfiId) | EECFI::CfiId | [protected] |
resetWarning() | EECFI::CfiClass | [static] |
satId() const | EECFI::Attitude | |
setData(const AttitudeData &attitudeData) | EECFI::Attitude | |
setTransformations(const TimeCorrelation &timeId, const SatNomTransId &satNomTrId, const SatTransId &satTrId, const InstrTransId &instTrId) | EECFI::Attitude | |
setWarning() | EECFI::CfiClass | [static] |
status() const | EECFI::CfiId | |
subtractInstance() | EECFI::CfiId | [protected] |
throwWarn | EECFI::CfiClass | [protected, static] |
userSet(const ModelId &modelId, const StateVector &stateVector, long targetFrame, const double matrix[3][3], const double matrixRate[3][3], const double matrixRateRate[3][3], const double offset[3]) | EECFI::Attitude | |
~Attitude() EXCEPT | EECFI::Attitude | |
~CfiClass() EXCEPT | EECFI::CfiClass | |
~CfiId() NOEXCEPT | EECFI::CfiId |