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- 外本 伸治
- 九州大学大学院工学研究院航空宇宙工学部門
書誌事項
- タイトル別名
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- A Study on Orbital Transfer of a Rigid Satellite System Using Its Nonholonomic Constraint
- ヒホロノミックセイ オ リヨウ シタ ゴウタイ エイセイ ノ キドウ ヘンコウ ニ カンスル ケンキュウ
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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.
収録刊行物
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- 日本航空宇宙学会論文集
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日本航空宇宙学会論文集 54 (634), 477-484, 2006
一般社団法人 日本航空宇宙学会
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詳細情報 詳細情報について
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- CRID
- 1390282679446960896
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- NII論文ID
- 10018429067
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- NII書誌ID
- AA11307372
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- ISSN
- 24323691
- 13446460
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- NDL書誌ID
- 8579983
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- 本文言語コード
- ja
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- データソース種別
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- JaLC
- NDL
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- CiNii Articles
- KAKEN
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- 抄録ライセンスフラグ
- 使用不可