WEKO3
アイテム
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Design of attitude control system for H2A-piggy solar sail spacecraft
https://jaxa.repo.nii.ac.jp/records/7445
https://jaxa.repo.nii.ac.jp/records/74451a4b259b-956b-43c9-a176-4b6cdf23f247
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Design of attitude control system for H2A-piggy solar sail spacecraft | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 姿勢制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | リアクション制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 推進薬消費 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ソーラーセイル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衛星設計 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | H-2Aロケット | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 位置敏感型検出器 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | PSD | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ニューテーション能動制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ANC | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 太陽センサ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | スピン安定化 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 推進薬 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衛星制御 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | attitude control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | reaction control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | propellant consumption | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | solar sail | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | numerical analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | satellite design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | H-2A rocket | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | position sensitive detector | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | PSD | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | active nutation control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ANC | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | solar sensor | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spin stabilization | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | propellant | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | satellite control | |||||
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 | |||||
その他のタイトル | ||||||
その他のタイトル | H2A-piggyソーラーセイル探査機の姿勢制御設計 | |||||
著者 |
岡田, 俊輔
× 岡田, 俊輔× 白澤, 洋次× 三和, 裕一× 森, 治× 川勝, 康弘× 津田, 雄一× 山本, 高行× 船瀬, 龍× 川口, 淳一郎× Okada, Shunsuke× Shirasawa, Yoji× Miwa, Yuichi× Mori, Osamu× Kawakatsu, Yasuhiro× Tsuda, Yuichi× Yamamoto, Takayuki× Funase, Ryu× Kawaguchi, Junichiro |
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著者所属 | ||||||
東京大学 大学院 | ||||||
著者所属 | ||||||
東京大学 大学院 | ||||||
著者所属 | ||||||
東京大学 大学院 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属(英) | ||||||
en | ||||||
University of Tokyo Graduate School | ||||||
著者所属(英) | ||||||
en | ||||||
University of Tokyo Graduate School | ||||||
著者所属(英) | ||||||
en | ||||||
University of Tokyo Graduate School | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
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/ISAS) | |||||
書誌情報 |
第17回アストロダイナミクスシンポジウム講演後刷り集 2007 en : Proceedings of 17th Workshop on JAXA Astrodynamics and Flight Mechanics p. 41-45, 発行日 2008-03 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | ISAS/JAXAではソーラーセイル探査機に関する研究を行っている。その一環として、H2Aロケットによるピギーバック衛星として10kg程度の探査機を打ち上げ、惑星間空間においてソーラーセイルによる太陽光子推進を実証する計画を進めている。本研究では、このミッションにおける各フェーズで必要となる姿勢制御について検討した。このミッションのフェーズは、(1)H2Aからの分離とGTO(Geostationary Transfer Orbit)軌道への投入、(2)固体モータによる惑星間軌道への投入、(3)ソーラーセイル膜の展開と光子推進の実証、の3つに大きく分けることができる。このそれぞれに対応した姿勢制御法を設計し、数値解析によって検証した。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | ISAS/JAXA is studying on the solar sail spacecraft for the future deep space explorations. As a part of the plan, we develop the probe whose weight is almost 10 kg. The main purpose of this mission is to verify the photon propulsion of solar sail at the interplanetary space. This probe is planed to be launched by H2A as piggyback. The mission consists of three stages: (1) separation from H2A and injection into GTO (Geostationary Transfer Orbit), (2) delta-V by the deorbit motor, and (3) deployment of the membrane and verification of the photon propulsion. This paper discusses the attitude control system of the mission. The attitude motion of the probe in each stage is different. The alignment of the thrusters and the sensors are designed to be optimal through the all stages. Using this alignment, the attitude control laws are proposed. The feasibility of the mission is examined by numerical simulation. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063718008 |