非ホロノミック性を利用した剛体衛星の軌道変更に関する研究

研究成果: Contribution to journalArticle査読

抄録

This study deals with orbital transfer of a rigid satellite system into a specified orbit by using its inner force generated in the system. First, the governing equations of the system are shown, and their non-integrability is proven by applying a nonlinear control theory. Subsequently, it is also shown that the system is controllable except its pericenter and its apocenter in an elliptic orbit. Then, this paper proposes a two-step approach, combining a solution for a ‘chained’ system and numerical modification based on ‘motion planning.’ Finally, computational simulations verify that orbital transfer to a specified orbit is accomplished successfully by applying the proposed approach.
寄稿の翻訳タイトルA Study on Orbital Transfer of a Rigid Satellite System Using Its Nonholonomic Constraint
本文言語Japanese
ページ(範囲)477-484
ページ数8
ジャーナル日本航空宇宙学会論文集 = Journal of the Japan Society for Aeronautical and Space Sciences
54
634
DOI
出版ステータス出版済み - 11 5 2006

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