{"created":"2023-06-20T14:40:28.794215+00:00","id":7367,"links":{},"metadata":{"_buckets":{"deposit":"defc2fa2-b096-42a3-b88e-594d885c2ae8"},"_deposit":{"created_by":1,"id":"7367","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7367"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007367","sets":["1543:1544:1554","1887:1891"]},"author_link":["39000","38999"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"はやぶさ帰還における軌道計画"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2010-03","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"2009","bibliographic_titles":[{"bibliographic_title":"アストロダイナミクスシンポジウム講演後刷り集"},{"bibliographic_title":"Proceedings of 19th workshop on JAXA Astrodynamics and Flight Mechanics","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"アストロダイナミクスシンポジウム (2009年7月30-31日. 宇宙航空研究開発機構宇宙科学研究本部))","subitem_description_type":"Other"}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"Workshop on JAXA Astrodynamics and Flight Mechanics, 2009 (July 30-31, 2009. Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"摘要: 小惑星探査機「はやぶさ」は2009 年7 月現在、地球に向けて航行中である。化学スラスタの故障などにより地球帰還が当初の予定から3 年遅れたが、220m/sのDeltaV量で地球帰還が可能である。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Hayabusa is asteroid explorer of Japan and it is on the way to the Earth return. In earth return phase, it uses two-stage optimization for trajectory synthesis. The malfunction of chemical thruster caused three years delay of Earth return. However, using multi stage optimization, it is possible to find the new return orbit easily. According to the latest orbit plan, the remain delta-V is only 220m/s.","subitem_description_type":"Other"}]},"item_5_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"}]},"item_5_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0064734062","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)"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11567475","subitem_source_identifier_type":"NCID"}]},"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"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"NEC Aerospace Systems"}]},"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":"松岡, 正敏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsuoka, Masatoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"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 TRAJECTORY SYNTHESIS AND RESULTS IN EARTH RETURN PHASE","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"HAYABUSA TRAJECTORY SYNTHESIS AND RESULTS IN EARTH RETURN PHASE","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1554","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7367","relation_version_is_last":true,"title":["HAYABUSA TRAJECTORY SYNTHESIS AND RESULTS IN EARTH RETURN PHASE"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:40:36.959016+00:00"}