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PMAによる大型宇宙構造物の振動制御
https://jaxa.repo.nii.ac.jp/records/45373
https://jaxa.repo.nii.ac.jp/records/45373bfb0f3b1-59a3-4aae-b959-38317f904a11
名前 / ファイル | ライセンス | アクション |
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naltr01114.pdf (1.8 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | PMAによる大型宇宙構造物の振動制御 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | large space structures; proof mass actuator; robust stability; vibrational control | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Damping Enhancement of Large Space Structures by Proof-Mass-Actuators | |||||
著者 |
木田, 隆
× 木田, 隆× 山口, 功× 上野, 誠也× 田中, 正樹× KIDA, Takashi× Isao, Yamaguchi× Seiya, Ueno× Masaki, Tanaka |
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著者所属 | ||||||
航空宇宙技術研究所宇宙研究グループ | ||||||
著者所属 | ||||||
航空宇宙技術研究所宇宙研究グループ | ||||||
著者所属 | ||||||
横浜国立大学 | ||||||
著者所属 | ||||||
株式会社東芝 | ||||||
著者所属(英) | ||||||
en | ||||||
Space Technology Research Group, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Space Technology Research Group, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Yokohama National University | ||||||
著者所属(英) | ||||||
en | ||||||
TOSHIBA Corporation | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory(NAL) | |||||
書誌情報 |
航空宇宙技術研究所報告 en : Technical Report of National Aerospace Laboratory TR-1114 巻 1114, p. 19, 発行日 1991-05 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 本論文は大型宇宙構造物LSSの構造減衰を能動的に増加する制御技術について述べる。このために,PMAとよばれるアクチュエータを設計・試作した。このPMAを使用して,構造減衰を達成するときの閉ループ系の安定条件をまず検討する。そして1入力1出力系,2入力2出力系の2つの場合の構造減衰の実験結果を示す。最後に,PMAのサイジングについて考察する。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The enhancement of modal damping is a key technology in Large Space Structures (LSS) robust control. A controller design is examined which augments substantial damping factors to LSS actively. The stability analysis of the closed-loop system is first discussed, being subsequently confirmed by a ground-based control experiment which used a newly developed pivoted type Proof Mass Actuator (PMA). The controller utilizes a direct velocity feedback control. A multi-input multi-output control system was examined using two PMAs, in addition to the single-input single-output case. In both cases, the experimental results showed excellent vibration suppression capability. A sizing problem of the PMAs is also discussed. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTR1114000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL TR-1114 |