| Earth Observation Mission CFI Software Pointing Software User Manual for JAVA |

# EECFI.Attitude Member List

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

Attitude() | EECFI.Attitude |
Attitude(final TimeCorrelation timeId, final SatNomTransId satNomTrId, final SatTransId satTrId, final InstrTransId instTrId) | EECFI.Attitude |
CfiClass() | EECFI.CfiClass |
CfiId() | EECFI.CfiId |
CfiId(CfiId cfiId) | EECFI.CfiId |
changeFrame(final SatId satId, final ModelId modelId, long modeFlag, long frameFlagIn, long frameIdIn, long frameFlagOut, long frameIdOut, final StateVector satStateVec, final Coord statVecIn) | EECFI.Attitude |
compute(final ModelId modelId, final StateVector stateVector, long targetFrame) | EECFI.Attitude |
eq(final Attitude att) | EECFI.Attitude |
EECFI::CfiId.eq(CfiId cfiId) | EECFI.CfiId |
getData() | EECFI.Attitude |
mode() | EECFI.CfiId |
resetWarning() | EECFI.CfiClass |
setData(final AttitudeData attitudeData) | EECFI.Attitude |
setTransformations(final TimeCorrelation timeId, final SatNomTransId satNomTrId, final SatTransId satTrId, final InstrTransId instTrId) | EECFI.Attitude |
setWarning() | EECFI.CfiClass |
status() | EECFI.CfiId |
userSet(final ModelId modelId, final StateVector stateVector, long targetFrame, final double[][] matrix, final double[][] matrixRate, final double[][] matrixRateRate, final double[] offset) | EECFI.Attitude |