{"created":"2023-06-20T14:40:35.590160+00:00","id":7502,"links":{},"metadata":{"_buckets":{"deposit":"95dd6523-1f8e-4bbd-8334-cba55ba21f20"},"_deposit":{"created_by":1,"id":"7502","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7502"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007502","sets":["1543:1544:1557","1887:1891"]},"author_link":["40026","40028","40025","40027"],"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2007-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"6","bibliographicPageStart":"1","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":"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。このSCOPEで想定されている軌道は近地点距離+3,000km、遠地点距離30程度の長楕円軌道である。一般に地球周回軌道での編隊飛行では月の影響はほとんど考慮しないが、SCOPEで想定されているような長楕円軌道になってくるとその摂動効果が無視できないものとなってくる。本稿では月摂動を考慮した編隊飛行の運動方程式を導出し、その周期性を利用した半解析的手法を用いて月摂動の影響を調べる。さらに数値シミュレーションを行い、用いた解析法の妥当性を検証する。","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 mother satellite and four daughters. The planned orbit of the SCOPE mission is a highly elliptic orbit with Re+3,000 km perigee and 30 Re apogee. In general, the effect of the lunar perturbation on the relative dynamics of formation flying spacecrafts is negligible in low earth orbit. However in highly elliptic orbit, the effect becomes large and needs to be considered. This paper investigates the effect of the lunar perturbation on the formation flight dynamics in a half analytical way, and compares it with the result of numerical simulation to evaluate the validity of the analysis.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063481001","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":"東京大学"},{"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":"University of Tokyo"},{"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":"岡田, 俊輔"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"津田, 雄一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Okada, Shunsuke","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tsuda, Yuichi","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":"軌道計算","subitem_subject_scheme":"Other"},{"subitem_subject":"楕円軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"編隊飛行","subitem_subject_scheme":"Other"},{"subitem_subject":"地球磁気圏","subitem_subject_scheme":"Other"},{"subitem_subject":"運動方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"月効果","subitem_subject_scheme":"Other"},{"subitem_subject":"フロケの定理","subitem_subject_scheme":"Other"},{"subitem_subject":"摂動","subitem_subject_scheme":"Other"},{"subitem_subject":"月重力効果","subitem_subject_scheme":"Other"},{"subitem_subject":"数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"参照軌道","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":"orbit calculation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"elliptical orbit","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"formation flying","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Earth magnetosphere","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"equation of motion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"lunar effect","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Floquet theorem","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"perturbation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"lunar gravitational effect","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reference orbit","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":"The effect of perturbation by the Moon in a highly elliptic orbital formation flight","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"The effect of perturbation by the Moon in a highly elliptic orbital formation flight","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":"7502","relation_version_is_last":true,"title":["The effect of perturbation by the Moon in a highly elliptic orbital formation flight"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:38:32.578534+00:00"}