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 | 日本語 |
| 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 |
| 巻 | 54 |
| 号 | 634 |
| DOI | |
| 出版ステータス | 出版済み - 11月 5 2006 |