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Control of Electromagnetic Current at Final Docking Phase of Small Satellites
https://jaxa.repo.nii.ac.jp/records/22425
https://jaxa.repo.nii.ac.jp/records/22425b062cc2e-3933-4e69-a48f-e4d19c0b3d9d
Item type | 学術雑誌論文 / Journal Article(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Control of Electromagnetic Current at Final Docking Phase of Small Satellites | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Small Satellite; Position and Attitude Control; Formation Flight; Electro Magnet Force; Docking | |||||
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 | |||||
著者 |
Torisaka, Ayako
× Torisaka, Ayako× 小澤, 悟× Yamakawa, Hiroshi× Kobayashi, Nobuyuki× Torisaka, Ayako× Ozawa, Satoru× Yamakawa, Hiroshi× Kobayashi, Nobuyuki |
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著者所属 | ||||||
青山学院大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
早稲田大学 | ||||||
著者所属 | ||||||
青山学院大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Aoyama Gakuin University | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Waseda University | ||||||
著者所属(英) | ||||||
en | ||||||
Aoyama Gakuin University | ||||||
出版者 | ||||||
出版者 | 日本機械学会 | |||||
書誌情報 |
en : Journal of Space Engineering 巻 6, 号 1, p. 44-55, 発行日 2013-12 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper proposes a relative position and attitude control method by using onlymagnetic force with multi-dipole for formation-flying spacecrafts. The controlmethod can be widely applied to re-configurable space structures that architect largestructure or reconstruct themselves by assembling basic structural units. Oneremarkable benefit of the method is that it does not require reaction wheels forrelative attitude controls and then doesn't require any fuel for unloading. This paperfocuses on current control of dipoles which produce strong nonlinear magneticforces and suggests a way of linearization by using a corresponding linear referencesystem. A feasibility of this method and controllability of the strong nonlinearsystem is discussed, and then the series of position and attitude control simulationare shown, and the future works are suggested in the paper. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1881-736X | |||||
DOI | ||||||
識別子タイプ | DOI | |||||
関連識別子 | http://dx.doi.org/10.1299/spacee.6.44 | |||||
関連名称 | info:doi/10.1299/spacee.6.44 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: PA1410061000 |