{"created":"2023-06-20T14:40:24.958570+00:00","id":7294,"links":{},"metadata":{"_buckets":{"deposit":"f160ac30-17f1-4cee-9b74-f6378e87baca"},"_deposit":{"created_by":1,"id":"7294","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7294"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007294","sets":["1543:1544:1553","1887:1891"]},"author_link":["38544","38545"],"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2011-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"301","bibliographicPageStart":"284","bibliographicVolumeNumber":"20","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":"The 20th 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":"第20回アストロダイナミクスシンポジウム (2010年7月26-27日. 宇宙航空研究開発機構宇宙科学研究所), 相模原市, 神奈川県　","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":"The 20th Workshop on JAXA Astrodynamics and Flight Mechanics 2010 (July 26-27, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Slightly different from the commonly used term formation flying, cluster flying requires less control effort but a collision free orbit design for a multiple satellite configuration. In addition, fractionating a spacecraft and letting the different subsystems fly separately leads to the cluster flying design with the constraints of inter-satellite distances and visibility due to inter-satellite power transfer link requirement. In this manner, parallel separation of eccentricity and inclination vector method was used to design collision free relative orbits for a network of more than two satellites. Based on this method, three configurations were identified in terms of safety, visibility and combination of those. In this orbit design study, the optimization and evaluations of these configurations were presented. It was concluded that a safe, fuel efficient and close proximity cluster flying can be realized for a fractionated spacecraft with respect to a given set of constraints.","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: AA0065115047","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所 (JAXA)(ISAS)"}]},"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_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":"東京大学工学部航空宇宙工学科中須賀研究室"},{"subitem_text_value":"東京大学工学部航空宇宙工学科中須賀研究室"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Intelligent Space Systems Laboratory, Department of Aeronautics and Astronautics, University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"Intelligent Space Systems Laboratory, Department of Aeronautics and Astronautics, University of Tokyo"}]},"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":"Yaglioglu, Burak","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Wang, Jihe","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":"Cluster Flying Configuration Evaluation in the Case of Fractionated Spacecraft Architecture","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Cluster Flying Configuration Evaluation in the Case of Fractionated Spacecraft Architecture","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1553","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7294","relation_version_is_last":true,"title":["Cluster Flying Configuration Evaluation in the Case of Fractionated Spacecraft Architecture"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:41:44.141519+00:00"}