{"created":"2023-06-20T14:40:33.892624+00:00","id":7473,"links":{},"metadata":{"_buckets":{"deposit":"4dc1505c-66d1-49c6-a4eb-d57a84ada6cd"},"_deposit":{"created_by":1,"id":"7473","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7473"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007473","sets":["1543:1544:1556","1887:1891"]},"author_link":["39824","39821","39826","39825","39822","39823"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"楕円軌道のフォーメーションフライトにおける擾乱の影響"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2008-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"223","bibliographicPageStart":"218","bibliographic_titles":[{"bibliographic_title":"第17回アストロダイナミクスシンポジウム講演後刷り集　2007"},{"bibliographic_title":"Proceedings of 17th Workshop on JAXA Astrodynamics and Flight Mechanics","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"楕円軌道回りのフォーメーションフライトにおける、J(sub 2)項による外乱の影響について考察する。フォーメーション軌道における宇宙機の相対運動は外乱の影響によって徐々に変動をうけるが、この変動を抑えるような相対運動の初期条件の与え方について検討する。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper proposes a basic method for constructing a formation flight around an eccentric reference orbit under the J(sub 2) influences. The relative motion between two spacecraft in the formation flight is affected by the gravitational disturbance J(sub 2). The effects of this perturbing force are analyzed and initial conditions of the formation flight to suppress these effects are derived based on the analytical results.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063718036","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":"名古屋大学"},{"subitem_text_value":"三菱電機"},{"subitem_text_value":"三菱電機"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Nagoya University"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Electric Corporation"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Electric Corporation"}]},"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":"山田, 克彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"島, 岳也"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"吉河, 章二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamada, Katsuhiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shima, Takeya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yoshikawa, Shoji","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"編隊飛行","subitem_subject_scheme":"Other"},{"subitem_subject":"重力場","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星擾乱","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"楕円軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"擾乱","subitem_subject_scheme":"Other"},{"subitem_subject":"地球重力","subitem_subject_scheme":"Other"},{"subitem_subject":"軌跡","subitem_subject_scheme":"Other"},{"subitem_subject":"離心率","subitem_subject_scheme":"Other"},{"subitem_subject":"シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"重力擾乱","subitem_subject_scheme":"Other"},{"subitem_subject":"J(sub 2)効果","subitem_subject_scheme":"Other"},{"subitem_subject":"ヒル座標","subitem_subject_scheme":"Other"},{"subitem_subject":"参照軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"formation flying","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"gravitational field","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite perturbation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft trajectory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"elliptical orbit","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"perturbation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Earth gravitation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"trajectory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"eccentricity","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"gravitational disturbance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"J(sub 2) effect","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Hill coordinate","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":"Effects of perturbation in formation flight around an eccentric reference orbit","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Effects of perturbation in formation flight around an eccentric reference orbit","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1556","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7473","relation_version_is_last":true,"title":["Effects of perturbation in formation flight around an eccentric reference orbit"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:38:59.424765+00:00"}