Three body problem of planetary orbiters based on central body oblateness, solar effects, and atmospheric drag using equations of motion and transformations
Variation of parameters and the long-term behavior of planetary orbiters. Part 1 - Theory
1970-02-01
Report
No indication
English
VLBA Astrometry of Planetary Orbiters
NTRS | 2012
|Orbit evaluation technique for planetary orbiters
AIAA | 1968
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