書誌事項
- タイトル別名
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- Feedback Control of Orbital Parameters for a Rigid Satellite under Nonholonomic Constraint
- ヒホロノミック コウソク ニ チャクモクシタ ゴウタイ エイセイ キドウ ノ フィードバック セイギョ
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抄録
This study proposes a feedback control law for orbital parameters of a coplanar rigid satellite system. The governing equations are denoted as ‘Symmetrical Affine System’ with three variables and two control inputs, which is guaranteed to be locally controllable. However, because of time-variant parameters included in the governing equations, previously proposed feedback control laws cannot be directly applied. Therefore, in this paper, a novel feedback control law to simultaneously control plural orbital parameters is proposed. Finally the effectiveness of the proposed control law is validated through numerical simulations.
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 56 (648), 1-7, 2008
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
- 1390282679447125376
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- NII論文ID
- 10021152766
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- NII書誌ID
- AA11307372
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- ISSN
- 24323691
- 13446460
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- NDL書誌ID
- 9351562
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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
- Crossref
- CiNii Articles
- KAKEN
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- 抄録ライセンスフラグ
- 使用不可