@inproceedings{oai:jaxa.repo.nii.ac.jp:00007766,
 author = {津田, 雄一 and 中須賀, 真一 and Tsuda, Yuichi and Nakasuka, Shinichi},
 book = {平成14年度アストロダイナミクスシンポジウム:講演後刷り集, ISAS Proceedings of 12th Workshop on Astrodynamics and Flight Mechanics 2002: A Collection of Technical Papers},
 month = {Feb},
 note = {フォーメーションフライトにおいて、待機中ないしミッション休止中に、各衛星を一定領域内に留めておく技術は、所定の形状へ隊形を変更するのと同等に重要である。本稿では、長期にわたって各衛星が無制御で一定領域内に留まっているような軌道を待機軌道と呼び、その力学的性質およびそれを利用した最適誘導則の検討を行なう。, In the formation flight, one of the important guidance techniques besides formation changing is to make the member satellites stay within a certain area during a stand-by phase in a mission or a down-time between missions. Let the orbits staying within a certain distance with each other without control a 'stand-by orbit'. This paper describes the dynamical characteristics of the stand-by orbit and derives an optimal guidance law to insert onto it., 資料番号: AA0045497004},
 pages = {23--28},
 publisher = {宇宙科学研究所, The Institute of Space and Astronautical Science (ISAS)},
 title = {Optimal guidance law for stand-by orbit insertion for formation flying spacecraft},
 year = {2003}
}