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Earth Observation Mission CFI Software Orbit Software User Manual for JAVA |
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| 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 |
1.7.1