{"created":"2023-06-20T14:40:35.968739+00:00","id":7511,"links":{},"metadata":{"_buckets":{"deposit":"328ced84-d4d2-44e8-b086-30beb7d69d94"},"_deposit":{"created_by":1,"id":"7511","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7511"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007511","sets":["1543:1544:1557","1887:1891"]},"author_link":["40061","40062","40060","40059"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"月同期軌道を用いたロバストな月周回軌道投入について"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2007-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"60","bibliographicPageStart":"55","bibliographic_titles":[{"bibliographic_title":"第16回アストロダイナミクスシンポジウム講演後刷り集　2006"},{"bibliographic_title":"Proceedings of 16th Workshop on JAXA Astrodynamics and Flight Mechanics","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"月探査ミッションにおいて、月周回軌道投入はもっとも重要なイベントである。軌道投入が正常に実施されない場合、探査機は月を通過し月重力圏から脱出してしまうばかりか、条件によっては月スイングバイによる加速により地球重力圏からも脱出してしまい、ミッション喪失につながる。本発表で提案する方法は、軌道投入が正常に実施されない場合でも、探査機が月と再会合するような軌道(月同期軌道)に投入されるように、軌道を設計するというものである。講演では、このような軌道の設計方法と、それに基づく軌道設計例を示す。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Discussed in this paper is a lunar approach strategy tolerant of Lunar Orbit Injection (LOI) failure. LOI is one of the most critical events for a lunar orbiting mission. If the injection is not performed, the spacecraft flies by the moon, and in the worst case, it escapes not only from the moon but also from the earth, which leads to the mission failure. The proposed strategy is to design the trajectory so as to provide the opportunity and condition for the mission recovery even in the case of unexpected fly-by. That is, to design the trajectory so as to re-encounter the moon even in the case that the LOI is not performed. The trajectory design procedure is introduced and an example of designed trajectory is shown.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063481010","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":"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 総合技術研究本部"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Aerospace Technology"}]},"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":"川勝, 康弘"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山本, 昌幸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kawakatsu, Yasuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamamoto, Masayuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"月周回軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道投入","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道計算","subitem_subject_scheme":"Other"},{"subitem_subject":"遷移軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"スイングバイ技術","subitem_subject_scheme":"Other"},{"subitem_subject":"月同期軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"MSO","subitem_subject_scheme":"Other"},{"subitem_subject":"月周回軌道投入","subitem_subject_scheme":"Other"},{"subitem_subject":"LOI","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道設計","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道最適化","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道変換","subitem_subject_scheme":"Other"},{"subitem_subject":"ロバスト性","subitem_subject_scheme":"Other"},{"subitem_subject":"月探査","subitem_subject_scheme":"Other"},{"subitem_subject":"lunar orbit","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbit injection","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbit calculation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transfer orbit","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"swingby technique","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"moon synchronous orbit","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"MSO","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"lunar orbit injection","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"LOI","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"trajectory design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"trajectory optimization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite orbit","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbital maneuver","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"robustness","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"lunar exploration","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":"Robust lunar orbit injection by the usage of moon synchronous orbit","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Robust lunar orbit injection by the usage of moon synchronous orbit","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1557","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7511","relation_version_is_last":true,"title":["Robust lunar orbit injection by the usage of moon synchronous orbit"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:38:23.478526+00:00"}