Expansion of the Third-Body Disturbing Function
- 1 May 1981
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 4 (3) , 346-348
- https://doi.org/10.2514/3.19740
Abstract
No abstract availableKeywords
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- Equinoctial orbit elements - Application to artificial satellite orbitsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Existence of quasi-periodic solutions to the three-body problemCelestial Mechanics and Dynamical Astronomy, 1971