Abstract
This paper discusses the stability of the pseudo orbit, which flies outside of the sphere of influence of the secondary body in the Circular Restricted Three-Body Problem and has the same semi-major axis as the secondary body and a small eccentricity. The whole aspect of the stability of the inclined pseudo orbit is resolved for the first time by both examination using virtual energy and reduction to Mathieu's equation.
| Original language | English |
|---|---|
| Pages (from-to) | 1691-1698 |
| Number of pages | 8 |
| Journal | Advances in the Astronautical Sciences |
| Volume | 108 II |
| Publication status | Published - 2001 |
| Externally published | Yes |
| Event | Proceedings of the AAS/AIAA Space Flight Mechanics Meeting - Santa Barbara, CA, United States Duration: 2001 Feb 11 → 2001 Feb 15 |
ASJC Scopus subject areas
- Aerospace Engineering
- Space and Planetary Science