{"created":"2023-06-20T14:40:32.653018+00:00","id":7445,"links":{},"metadata":{"_buckets":{"deposit":"0c1d83ba-9e3e-406f-822c-9f6574c51c70"},"_deposit":{"created_by":1,"id":"7445","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7445"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007445","sets":["1543:1544:1556","1887:1891"]},"author_link":["39622","39625","39630","39632","39637","39635","39624","39636","39628","39623","39629","39638","39631","39633","39626","39634","39639","39627"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"H2A-piggyソーラーセイル探査機の姿勢制御設計"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2008-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"45","bibliographicPageStart":"41","bibliographic_titles":[{"bibliographic_title":"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"},{"bibliographic_title":"Proceedings of 17th Workshop on JAXA Astrodynamics and Flight Mechanics","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"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。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"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.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063718008","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構宇宙科学研究本部"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東京大学 大学院"},{"subitem_text_value":"東京大学 大学院"},{"subitem_text_value":"東京大学 大学院"},{"subitem_text_value":"宇宙航空研究開発機構 宇宙科学研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 宇宙科学研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 宇宙科学研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 宇宙科学研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 宇宙科学研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 宇宙科学研究本部"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"University of Tokyo Graduate School"},{"subitem_text_language":"en","subitem_text_value":"University of Tokyo Graduate School"},{"subitem_text_language":"en","subitem_text_value":"University of Tokyo Graduate School"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"metadata only access","subitem_access_right_uri":"http://purl.org/coar/access_right/c_14cb"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"岡田, 俊輔"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"白澤, 洋次"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"三和, 裕一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"森, 治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"川勝, 康弘"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"津田, 雄一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山本, 高行"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"船瀬, 龍"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"川口, 淳一郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Okada, Shunsuke","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shirasawa, Yoji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Miwa, Yuichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Mori, Osamu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kawakatsu, Yasuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tsuda, Yuichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamamoto, Takayuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Funase, Ryu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kawaguchi, Junichiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"姿勢制御","subitem_subject_scheme":"Other"},{"subitem_subject":"リアクション制御","subitem_subject_scheme":"Other"},{"subitem_subject":"推進薬消費","subitem_subject_scheme":"Other"},{"subitem_subject":"ソーラーセイル","subitem_subject_scheme":"Other"},{"subitem_subject":"数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星設計","subitem_subject_scheme":"Other"},{"subitem_subject":"H-2Aロケット","subitem_subject_scheme":"Other"},{"subitem_subject":"位置敏感型検出器","subitem_subject_scheme":"Other"},{"subitem_subject":"PSD","subitem_subject_scheme":"Other"},{"subitem_subject":"ニューテーション能動制御","subitem_subject_scheme":"Other"},{"subitem_subject":"ANC","subitem_subject_scheme":"Other"},{"subitem_subject":"太陽センサ","subitem_subject_scheme":"Other"},{"subitem_subject":"スピン安定化","subitem_subject_scheme":"Other"},{"subitem_subject":"推進薬","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星制御","subitem_subject_scheme":"Other"},{"subitem_subject":"attitude control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reaction control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"propellant consumption","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solar sail","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"H-2A rocket","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"position sensitive detector","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"PSD","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"active nutation control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ANC","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solar sensor","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spin stabilization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"propellant","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite control","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"Design of attitude control system for H2A-piggy solar sail spacecraft","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Design of attitude control system for H2A-piggy solar sail spacecraft","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1556","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7445","relation_version_is_last":true,"title":["Design of attitude control system for H2A-piggy solar sail spacecraft"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:39:25.655943+00:00"}