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Stabilizing nonlinear control of spacecraft at capturing and docking phase
https://jaxa.repo.nii.ac.jp/records/7621
https://jaxa.repo.nii.ac.jp/records/76211f52f929-a398-465d-8045-1d56392a7d5a
Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Stabilizing nonlinear control of spacecraft at capturing and docking phase | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衛星制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衛星追跡 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | タンブリング運動 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 制御則 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 非線形制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙機捕捉 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | PD型制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙機ドッキング | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙機回収 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 制御系設計 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 安定化 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 制御理論 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 制御シミュレーション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | リアプノフ関数 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | satellite control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | satellite tracking | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | tumbling motion | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | control law | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | nonlinear control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spacecraft capturing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | PD-type control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spacecraft docking | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spacecraft recovery | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | control system design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | stabilization | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | control theory | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | control simulation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Lyapunov function | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル | ||||||
その他のタイトル | 人工衛星の捕捉および結合時の安定化非線形制御 | |||||
著者 |
伊藤, 玲
× 伊藤, 玲× 池田, 裕一× 長塩, 知之× 木田, 隆× Ito, Akira× Ikeda, Yuichi× Nagashio, Tomoyuki× Kida, Takashi |
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著者所属 | ||||||
電気通信大学 大学院 | ||||||
著者所属 | ||||||
電気通信大学 大学院 | ||||||
著者所属 | ||||||
電気通信大学 | ||||||
著者所属 | ||||||
電気通信大学 | ||||||
著者所属(英) | ||||||
en | ||||||
University of Electro-Communications Graduate School | ||||||
著者所属(英) | ||||||
en | ||||||
University of Electro-Communications Graduate School | ||||||
著者所属(英) | ||||||
en | ||||||
University of Electro-Communications | ||||||
著者所属(英) | ||||||
en | ||||||
University of Electro-Communications | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究本部 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS) | |||||
書誌情報 |
第15回アストロダイナミクスシンポジウム講演後刷り集 2005 en : Proceedings of 15th Workshop on JAXA Astrodynamics and Flight Mechanics p. 358-363, 発行日 2006-03 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 将来の宇宙インフラストラクチャ構想において、衛星への燃料補給や故障衛星を回収するミッションが考えられている。それらを遂行するためにはターゲットに対し、チェイサーの接近、結合、捕捉が必要になるが、宇宙機の運動は回転と並進が干渉した非線形システムで表され、それを考慮した制御系を設計する必要がある。そこで本研究では人工衛星の捕捉および結合時における結合前後の安定条件を満たす非線形制御系の設計法を検討する。そして数値例によりその有効性を確認する。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In the future space infra-structure plan, the missions of spacecraft capturing and docking are considered. The motion of the spacecraft is described as the nonlinear system interfered of the rotation and translation dynamics. We derive the condition of the stabilizing controller for the nonlinear spacecraft system before and after docking and capturing. Then, its capability is investigated by numerical simulations. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063480056 |