Earth Observation Mission CFI Software Orbit Software User Manual for JAVA |
add(double time) | EECFI.ANXTime | |
adjustWithNodalPeriod() | EECFI.ANXTime | |
ANXTime() | EECFI.ANXTime | |
ANXTime(long orbitIn, long secondsIn, long microsecIn) | EECFI.ANXTime | |
ANXTime(final OrbitId orbitIdIn, long orbitIn, long secondsIn, long microsecIn) | EECFI.ANXTime | |
ANXTime(final ANXTime at) | EECFI.ANXTime | |
CfiClass() | EECFI.CfiClass | |
copy(final ANXTime at) | EECFI.ANXTime | |
eq(final ANXTime at) | EECFI.ANXTime | |
ge(final ANXTime at) | EECFI.ANXTime | |
getOrbitInfo() | EECFI.ANXTime | |
gt(final ANXTime at) | EECFI.ANXTime | |
le(final ANXTime at) | EECFI.ANXTime | |
lt(final ANXTime at) | EECFI.ANXTime | |
microseconds | EECFI.ANXTime | |
neq(final ANXTime at) | EECFI.ANXTime | |
orbit | EECFI.ANXTime | |
orbitInfoConfigure(long item, long option) | EECFI.ANXTime | |
orbitToTime(long timeRef) | EECFI.ANXTime | |
resetWarning() | EECFI.CfiClass | |
seconds | EECFI.ANXTime | |
setBOM() | EECFI.ANXTime | |
setEOM() | EECFI.ANXTime | |
setWarning() | EECFI.CfiClass | |
subtract(double time) | EECFI.ANXTime | |
subtract(final ANXTime at) | EECFI.ANXTime | |
timeToOrbit(long timeRef, double time) | EECFI.ANXTime |