{"created":"2023-06-20T14:40:48.991433+00:00","id":7765,"links":{},"metadata":{"_buckets":{"deposit":"7095d6f0-bb8b-40d9-8cca-8cbda48ea6fe"},"_deposit":{"created_by":1,"id":"7765","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7765"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007765","sets":["1543:1544:1561","1887:1891"]},"author_link":["41755","41756"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"長楕円軌道上フォーメーションフライトの軌道設計と制御に関する一考察"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2003-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"22","bibliographicPageStart":"16","bibliographic_titles":[{"bibliographic_title":"平成14年度アストロダイナミクスシンポジウム:講演後刷り集"},{"bibliographic_title":"ISAS Proceedings of 12th Workshop on Astrodynamics and Flight Mechanics 2002: A Collection of Technical Papers","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"現在宇宙科学研究所において、GEOTAIL衛星の後継機として複数衛星を用いたプラズマ磁気圏観測ミッションの検討が進められている(GEOTAIL-2)。複数の衛星を用いることで現象の空間変化を観測することができる。プラズマ観測では地心から地球半径の20倍から30倍離れた領域が観測対象となり、衛星の軌道は楕円軌道になる。楕円軌道上では、衛星間の相対位置は時間とともに大きく変化するため高い空間観測性を維持する軌道設計が重要となる。また、フォーメーションフライトのミッションではフォーメーションの崩壊を防ぐ事が重要となる。本考察では、軌道設計とフォーメーション維持制御の方法について示す。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"At the Institute of Space and Astronautical Science (ISAS), the plasma and magnetic field observation mission with several satellites is projected. The project under consideration is designated as GEOTAIL-2. It is named after the GEOTAIL satellite. By using the plural satellites, the observation with high space resolution become realizable. The plasma physics observation focuses its attention on the elliptic orbit whose apogee distance reaches to twenty or thirty earth radii. On such orbits with large eccentricity, the relative positions of the satellites change largely as time goes on. So the design of the orbit that keeps the high space resolution is necessary. And in these missions, it is important to maintain the formation. In this study, the method of the orbit design and formation maintenance control strategy in the elliptic orbit are shown.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0045497003","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙科学研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"The Institute of Space and Astronautical Science (ISAS)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0918-8053","subitem_source_identifier_type":"ISSN"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東京大学 大学院工学系研究科"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"University of Tokyo Graduate School of Engineering"}]},"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":"佐伯, 孝尚"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Saiki, Takanao","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"フォーメーションフライト","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道計算","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道設計","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道制御","subitem_subject_scheme":"Other"},{"subitem_subject":"楕円軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"GEOTAIL衛星","subitem_subject_scheme":"Other"},{"subitem_subject":"プラズマ圏","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙力学","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星配置","subitem_subject_scheme":"Other"},{"subitem_subject":"formation flight","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbit calculation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbital design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbit control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"elliptical orbit","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"GEOTAIL satellite","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"plasmasphere","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"astrodynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite constellation","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":"A study on the orbit design and control strategy for formation flying in the elliptic orbit","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"A study on the orbit design and control strategy for formation flying in the elliptic orbit","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1561","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7765","relation_version_is_last":true,"title":["A study on the orbit design and control strategy for formation flying in the elliptic orbit"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:34:25.426223+00:00"}