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.
|ジャーナル||Advances in the Astronautical Sciences|
|出版ステータス||Published - 2001|
|イベント||Proceedings of the AAS/AIAA Space Flight Mechanics Meeting - Santa Barbara, CA, United States|
継続期間: 2001 2 11 → 2001 2 15
ASJC Scopus subject areas