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Adaptive Control of Large Space Structure (LSS)
https://jaxa.repo.nii.ac.jp/records/31386
https://jaxa.repo.nii.ac.jp/records/3138609aac5cb-4495-408d-9e60-a77aeffe2e89
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
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| Item type | 紀要論文 / Departmental Bulletin Paper(1) | |||||||
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| 公開日 | 2015-03-26 | |||||||
| タイトル | ||||||||
| タイトル | Adaptive Control of Large Space Structure (LSS) | |||||||
| 言語 | en | |||||||
| 言語 | ||||||||
| 言語 | eng | |||||||
| 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 | departmental bulletin paper | |||||||
| 著者 |
Yu, SHAOHUA
× Yu, SHAOHUA
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| 出版者 | ||||||||
| 出版者 | 宇宙科学研究所 | |||||||
| 出版者(英) | ||||||||
| 出版者 | Institute of Space and Astronautical Science | |||||||
| 書誌情報 |
en : The Institute of Space and Astronautical Science report 巻 621, p. 1-38, 発行日 1987-03 |
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| 抄録(英) | ||||||||
| 内容記述タイプ | Other | |||||||
| 内容記述 | A set of closely related topics, concerning the methodology of an optimal attitude maneuver control of satellite with flexible appendages, has been investigated : Such as mathematic model of coupled motion, pulse-mode control, optimal and programed maneuver, appendages' vibration damping through adaptive control and conventional control, adaptive identification (deterministic and stochastic) algorithm of time-varying modal coordinate parameters. A distinctive feature of the research was that only the actuators of central satellite attitude control system were assumed to perform both satellite attitude control and appendages' deformation control. Some aspects of interaction between control system characteristics and structure/configuration design parameters were outlined. | |||||||
| ISSN | ||||||||
| 収録物識別子タイプ | ISSN | |||||||
| 収録物識別子 | 0285-6808 | |||||||
| 書誌レコードID | ||||||||
| 収録物識別子タイプ | NCID | |||||||
| 収録物識別子 | AA10632072 | |||||||
| 資料番号 | ||||||||
| 内容記述タイプ | Other | |||||||
| 内容記述 | 資料番号: SA0035015000 | |||||||