{"created":"2023-06-20T14:40:42.876091+00:00","id":7632,"links":{},"metadata":{"_buckets":{"deposit":"8eb55e42-5122-4ada-b0a1-787eb266d884"},"_deposit":{"created_by":1,"id":"7632","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7632"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007632","sets":["1543:1544:1558","1887:1891"]},"author_link":["40883","40889","40885","40888","40884","40887","40886","40890"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"SCOPEにおける編隊飛行のための測距システムと軌道設計"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2006-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"433","bibliographicPageStart":"429","bibliographic_titles":[{"bibliographic_title":"第15回アストロダイナミクスシンポジウム講演後刷り集　2005"},{"bibliographic_title":"Proceedings of 15th Workshop on JAXA Astrodynamics and Flight Mechanics","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"JAXA宇宙科学研究本部が2010年代の実現を目指して検討中の地球磁気圏観測衛星「SCOPE(cross-Scale COupling in Plasma universE)」は、5機の衛星が編隊飛行をしながら電磁場の同時観測を行うミッションである。SCOPEでは複数衛星間で観測データの相関処理を行うために、非常に高い時刻同期精度と相対位置決定精度が要求される。本稿では、SCOPEで現在検討中の相対軌道決定・時刻同期手法およびそれを実現するハードウェアの開発状況について紹介する。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Japan Aerospace Exploration Agency (JAXA) is currently planning the next generation magnetosphere observation mission called 'SCOPE.' (cross-Scale COupling in Plasma universE) SCOPE consists of five satellites, one 450 kg mother satellite and four 90 kg daughters, which are assumed to be launched by JAXA's M-V rocket at once. Five satellites fly in basically a tetrahedron formation, minimum 5 km apart from each other, at their perigee of 30 Earth-radii distance. To obtain the highly accurate spatial distribution of the magnetospheric phenomena, the quality of the clock synchronization and the relative orbit determination between satellites are essential. SCOPE satellites are to be equipped with the intersatellite communication and ranging system, which is now being developed, to realize the accuracy of 5 usec as to clock synchronization and 50 m as to the relative distance measurement for that purpose. This paper introduces the current orbit design and the ranging system of SCOPE to realize the highly accurate magnetotail formation flying mission.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063480067","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 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":"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":"津田, 雄一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"市川, 勉"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"戸田, 知朗"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"斎藤, 義文"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tsuda, Yuichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ichikawa, Tsutomu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Toda, Tomoaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Saito, Yoshifumi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"SCOPE","subitem_subject_scheme":"Other"},{"subitem_subject":"地球磁気圏観測衛星","subitem_subject_scheme":"Other"},{"subitem_subject":"編隊飛行","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道決定","subitem_subject_scheme":"Other"},{"subitem_subject":"位置決め","subitem_subject_scheme":"Other"},{"subitem_subject":"時計同期化","subitem_subject_scheme":"Other"},{"subitem_subject":"時分割多元接続","subitem_subject_scheme":"Other"},{"subitem_subject":"地球磁気圏","subitem_subject_scheme":"Other"},{"subitem_subject":"磁気圏尾部","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星搭載装置","subitem_subject_scheme":"Other"},{"subitem_subject":"測距","subitem_subject_scheme":"Other"},{"subitem_subject":"時計","subitem_subject_scheme":"Other"},{"subitem_subject":"M-Vロケット","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星間距離計測","subitem_subject_scheme":"Other"},{"subitem_subject":"SCOPE","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"cross-Scale COupling in Plasma universE","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"formation flying","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbit determination","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"positioning","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"clock synchronization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"time division multiple access","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Earth magnetosphere","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"magnetotail","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite-borne instrument","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rangefinding","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"clock","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"M-V rocket","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"intersatellite ranging","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":"Ranging system and orbit design of scope formation flying mission","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Ranging system and orbit design of scope formation flying mission","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1558","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7632","relation_version_is_last":true,"title":["Ranging system and orbit design of scope formation flying mission"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:36:28.920285+00:00"}