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大型柔軟衛星のロバスト姿勢制御(入力拘束を考慮したモデル予測制御の適用)
https://jaxa.repo.nii.ac.jp/records/22487
https://jaxa.repo.nii.ac.jp/records/224879a0742a1-04ab-42bc-9138-efa45ba4f27a
Item type | 学術雑誌論文 / Journal Article(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 大型柔軟衛星のロバスト姿勢制御(入力拘束を考慮したモデル予測制御の適用) | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Model Predictive Control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Robust Control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Input-Constraint | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Flexible Spacecraft | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Attitude Control | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | journal article | |||||
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(英) | ||||||
その他のタイトル | Robust Attitude Control of Large Flexible Spacecraft: Application of Input Constrained Model Predictive Control | |||||
著者 |
山下, 哲生
× 山下, 哲生× 濱田, 吉郎× 山口, 功× 長塩, 知之× 木田, 隆× Yamashita, Tetsuo× Hamada, Yoshiro× Yamaguchi, Isao× Nagashio, Tomoyuki× Kida, Takashi |
|||||
著者所属 | ||||||
電気通信大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構研究開発本部(JAXA) | ||||||
著者所属 | ||||||
防衛大学校 | ||||||
著者所属 | ||||||
大阪府立大学 | ||||||
著者所属 | ||||||
電気通信大学 | ||||||
著者所属(英) | ||||||
en | ||||||
The University of Electro-Communications (UEC) | ||||||
著者所属(英) | ||||||
en | ||||||
Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
National Defense Academy of Japan (NDA) | ||||||
著者所属(英) | ||||||
en | ||||||
Osaka Prefecture University | ||||||
著者所属(英) | ||||||
en | ||||||
The University of Electro-Communications (UEC) | ||||||
出版者 | ||||||
出版者 | 日本機械学会(JSME) | |||||
出版者(英) | ||||||
出版者 | The Japan Society of Mechanical Engineers (JSME) | |||||
書誌情報 |
日本機械学会論文集C編 en : Transactions of the Japan Society of Mechanical Engineers. C 巻 79, 号 802, p. 1935-1948, 発行日 2013-06-25 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper presents an application of the model predictive control to flexible spacecraft attitude maneuver. The objective of the study is to demonstrate an experimental feasibility of optimal attitude controllers suppressing the flexible appendage vibration under the actuator saturation. For the purpose, we study two approaches in the model predictive control framework. One is to use the frequency-shaped linear quadratic cost with finite horizon, and the other is to apply the robust control theory. Through ground experiments using a single axis air bearing table, as well as numerical studies for ETS-VIII spacecraft, their abilities are shown and compared. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0387-5024 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN00187463 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11553029 | |||||
DOI | ||||||
識別子タイプ | DOI | |||||
関連識別子 | http://dx.doi.org/10.1299/kikaic.79.1935 | |||||
関連名称 | info:doi/10.1299/kikaic.79.1935 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: PA1420038000 |