JAXA Space Exploration Center, Japan Aerospace Exploration Agency (JAXA)(JSPEC)
JAXA Space Exploration Center, Japan Aerospace Exploration Agency (JAXA)(JSPEC)
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) : JAXA Space Exploration Center, Japan Aerospace Exploration Agency (JAXA)(JSPEC)
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) : JAXA Space Exploration Center, Japan Aerospace Exploration Agency (JAXA)(JSPEC)
出版者
宇宙航空研究開発機構宇宙科学研究本部
出版者（英）
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)
雑誌名
アストロダイナミクスシンポジウム講演後刷り集
雑誌名(英)
Proceedings of 18th workshop on JAXA Astrodynamics and flight mechanics
巻
2008
発行年
2009-03
会議概要（会議名, 開催地, 会期, 主催者等）（英）
Symposium on Flight Mechanics and Astrodynamics 2008 (July 28-29, 2008. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan
The orbit design of two spacecraft for Mars exploration mission is discussed. We assume two orbiters, whose orbits are required to be orthogonal. After Mars orbit insertion, it will be needed to adjust their orbital planes and eccentricity vectors appropriately for required configuration under J(sub 2) perturbation. We discuss how to insert S/C into these orbits and how to maintain them.
2機の火星オービタの軌道設計に関する初期検討
