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Earth Observation Mission CFI Software Orbit Software User Manual for JAVA |
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Orbital information. More...
Public Member Functions | |
| OrbitalInfo () | |
| Empty constructor. | |
| OrbitalInfo (long absOrb, long repCyc, long cycLen, double mlstDriftIn, double mlstIn, double anxLon, double utc, double[] pos, double[] vel, double[] meanKepl, double[] oscKepl, double nodPeriod, double utcSMX) | |
| Constructor with parameters. | |
Public Attributes | |
| long | absOrbit |
| Absolute orbit. | |
| long | repCycle |
| Repeat cycle. | |
| long | cycLength |
| Cycle length. | |
| double | mlstDrift |
| MLST drift (seconds/day). | |
| double | mlst |
| Mean Local Solar Time (hours). | |
| double | phasing |
| Longitude at ascending node (deg). | |
| double | utcAnx |
| UTC time at ascending node (days, processing format). | |
| double[] | posAnx |
| Position at ascending node (m). | |
| double[] | velAnx |
| Velocity at Ascending node (m/s). | |
| double[] | meanKep |
| Mean keplerian elements. | |
| double[] | oscKep |
| Osculating keplerian elements. | |
| double | nodalPeriod |
| Nodal period of orbit (s). | |
| double | utcSmx |
| UTC time at Spacecraft Midnight [days, processing format]. | |
Orbital information.
| EECFI.OrbitalInfo.OrbitalInfo | ( | ) |
Empty constructor.
| EECFI.OrbitalInfo.OrbitalInfo | ( | long | absOrb, | |
| long | repCyc, | |||
| long | cycLen, | |||
| double | mlstDriftIn, | |||
| double | mlstIn, | |||
| double | anxLon, | |||
| double | utc, | |||
| double[] | pos, | |||
| double[] | vel, | |||
| double[] | meanKepl, | |||
| double[] | oscKepl, | |||
| double | nodPeriod, | |||
| double | utcSMX | |||
| ) |
Constructor with parameters.
Absolute orbit.
Cycle length.
| double [] EECFI.OrbitalInfo.meanKep |
Mean keplerian elements.
| double EECFI.OrbitalInfo.mlst |
Mean Local Solar Time (hours).
| double EECFI.OrbitalInfo.mlstDrift |
MLST drift (seconds/day).
Nodal period of orbit (s).
| double [] EECFI.OrbitalInfo.oscKep |
Osculating keplerian elements.
| double EECFI.OrbitalInfo.phasing |
Longitude at ascending node (deg).
| double [] EECFI.OrbitalInfo.posAnx |
Position at ascending node (m).
Repeat cycle.
| double EECFI.OrbitalInfo.utcAnx |
UTC time at ascending node (days, processing format).
| double EECFI.OrbitalInfo.utcSmx |
UTC time at Spacecraft Midnight [days, processing format].
| double [] EECFI.OrbitalInfo.velAnx |
Velocity at Ascending node (m/s).
1.7.1