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Experimental Study on Tether Actuator for Vibration Suppression of Tethered Space Solar Power Satellite
https://jaxa.repo.nii.ac.jp/records/7988
https://jaxa.repo.nii.ac.jp/records/7988ec09ec0a-32ee-40f6-bb43-0196c1862aa4
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 | Experimental Study on Tether Actuator for Vibration Suppression of Tethered Space Solar Power Satellite | |||||
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_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 | |||||
著者 |
藤井, 裕矩
× 藤井, 裕矩× Fan, Jixiang× Fujii, Hironori A.× Yano, Youki |
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著者所属 | ||||||
神奈川工科大学工学部機械工学科 | ||||||
著者所属 | ||||||
神奈川工科大学工学部機械工学科 : 日本大学大学院理工学研究科航空宇宙工学専攻 | ||||||
著者所属 | ||||||
神奈川工科大学工学部機械工学科 | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Mechanical Engineering, Kanagawa Institute of Technology : Department of Control Science and Engineering, Harbin Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Mechanical Engineering, Kanagawa Institute of Technology : Department of Aerospace Engineering, Nihon University | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Mechanical Engineering, Kanagawa Institute of Technology | ||||||
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) | |||||
書誌情報 |
宇宙エネルギーシンポジウム en : Space Energy Symposium 巻 29, 発行日 2010-02 |
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会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 第29回宇宙エネルギーシンポジウム(2010年2月26日, 宇宙航空研究開発機構宇宙科学研究本部相模原キャンパス) | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The twenty-ninth Space Energy Symposium (February 26, 2010, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Sagamihara) | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Experimental study is reported for vibration suppression on tethered flexible space structures like the tethered space solar power satellites (SSPS) by employing a micro tension actuator. In the experiment, a micro tension actua-tor is used to generate very small tension and control the structure vibration. The micro tension actuator employs with a very flexible arm connected to tether in order to overcome the penalty of nonlinear behavior of tether. The model employed is a tethered space solar satellite. The control performance of the micro tension actuator is examined in its performance to suppress flexible structure connected through tether. Results of the experiment have verified the validity of this controller and the ability is confirmed on the vibration suppression of the micro tension actuator. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: CD-ROM1枚 | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Note: One CD-ROM | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10324356 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0064737016 |