{"created":"2023-06-20T14:40:33.163292+00:00","id":7457,"links":{},"metadata":{"_buckets":{"deposit":"69904b51-d16a-4ae8-8f4b-197fc154c876"},"_deposit":{"created_by":1,"id":"7457","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7457"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007457","sets":["1543:1544:1556","1887:1891"]},"author_link":["39713","39712","39711","39706","39714","39707","39709","39710","39705","39708"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"はやぶさのΔV姿勢運用"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2008-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"125","bibliographicPageStart":"120","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":"小惑星探査機「はやぶさ(MUSES-C: Asteroid Sample-return Spacecraft)」は2007年4月から地球帰還のためのイオンエンジンによるΔVを開始した。昨年は太陽輻射圧を利用することで燃料を使わないスピン姿勢制御方式を確立し、太陽追尾を実施した。この方式を踏まえて、イオンエンジン運転時に発生する推力軸周りの外乱トルクと太陽輻射によるトルクを拮抗させて、太陽追尾をする3軸姿勢制御を確立し、地球帰還のためのΔV運用を開始した。本報告では姿勢制御をどのように実施したか飛行結果を交えて述べる。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Hayabusa (MUSES-C: Asteroid Sample-return Spacecraft) spacecraft started the homeward journey with an ion engine driven in April, 2007 aiming at the Earth return. In 2006, the fuel-free sun-tracking attitude control strategy was established and performed during spin stabilization. Then, the non-spin attitude control has been executed since February 2007. The key point is the balance of the solar radiation torque and the swirl torque of ion engine thrust. This paper reports how those attitude control strategies were carried out, showing flight results.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063718020","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":"NEC航空宇宙システム"},{"subitem_text_value":"NEC航空宇宙システム"},{"subitem_text_value":"NEC航空宇宙システム"},{"subitem_text_value":"NEC航空宇宙システム"},{"subitem_text_value":"日本電気"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"NEC Aerospace Systems Ltd."},{"subitem_text_language":"en","subitem_text_value":"NEC Aerospace Systems Ltd."},{"subitem_text_language":"en","subitem_text_value":"NEC Aerospace Systems Ltd."},{"subitem_text_language":"en","subitem_text_value":"NEC Aerospace Systems Ltd."},{"subitem_text_language":"en","subitem_text_value":"NEC Corporation"}]},"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":"小湊, 隆"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"白川, 健一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松岡, 正敏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"浦谷, 知恵"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"大島, 武"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kominato, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shirakawa, Kenichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsuoka, Masatoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Uratani, Chie","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Oshima, Takeshi","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":"スピン安定化","subitem_subject_scheme":"Other"},{"subitem_subject":"太陽輻射","subitem_subject_scheme":"Other"},{"subitem_subject":"イオンエンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"姿勢安定性","subitem_subject_scheme":"Other"},{"subitem_subject":"安定化","subitem_subject_scheme":"Other"},{"subitem_subject":"はやぶさ","subitem_subject_scheme":"Other"},{"subitem_subject":"MUSES-C","subitem_subject_scheme":"Other"},{"subitem_subject":"小惑星探査機","subitem_subject_scheme":"Other"},{"subitem_subject":"デルタV運用","subitem_subject_scheme":"Other"},{"subitem_subject":"太陽追尾","subitem_subject_scheme":"Other"},{"subitem_subject":"3軸安定化","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星向き","subitem_subject_scheme":"Other"},{"subitem_subject":"トルク","subitem_subject_scheme":"Other"},{"subitem_subject":"追尾","subitem_subject_scheme":"Other"},{"subitem_subject":"attitude control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spin stabilization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solar radiation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ion engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"attitude stability","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stabilization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Hayabusa","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"MUSES-C","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Asteroid Sample-return Spacecraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"delta-V operation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"sun tracking","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"three axis stabilization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite orientation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"torque","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"tracking","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":"Hayabusa attitude control for delta-V operations","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Hayabusa attitude control for delta-V operations","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":"7457","relation_version_is_last":true,"title":["Hayabusa attitude control for delta-V operations"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:39:14.514202+00:00"}