{"created":"2023-06-20T14:40:39.346944+00:00","id":7574,"links":{},"metadata":{"_buckets":{"deposit":"5308dee9-07d6-497d-88a8-858a75817233"},"_deposit":{"created_by":1,"id":"7574","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7574"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007574","sets":["1543:1544:1558","1887:1891"]},"author_link":["40536","40538","40535","40537","40540","40539"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"宇宙機間の相対位置の制御について"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2006-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"54","bibliographicPageStart":"47","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":"本稿では2機の宇宙機の編隊飛行制御について検討する。2インパルスによって編隊のサイズを大きくする場合を対象に、推薬消費が最小となるような相対的な軌道変更軌道をHill方程式に基づいて導出し、そのときの推薬量を求める。この軌道設計を数値的に検証する。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper proposes the basic method for constructing a formation flying. It proposes a trajectory design of minimum-fuel consumption for spacecraft relative position change by two impulses. Numerical studies of the formation construction are executed in order to verify the trajectory control.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063480009","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":"吉河, 章二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"島, 岳也"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamada, Katsuhiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yoshikawa, Shoji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shima, Takeya","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":"軌道制御","subitem_subject_scheme":"Other"},{"subitem_subject":"数学的解析","subitem_subject_scheme":"Other"},{"subitem_subject":"数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"相対運動","subitem_subject_scheme":"Other"},{"subitem_subject":"ヒルの方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"費用関数","subitem_subject_scheme":"Other"},{"subitem_subject":"遷移時間","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"推進薬消費","subitem_subject_scheme":"Other"},{"subitem_subject":"速度","subitem_subject_scheme":"Other"},{"subitem_subject":"最適化","subitem_subject_scheme":"Other"},{"subitem_subject":"formation flying","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"trajectory control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"mathematical analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"relative motion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Hill's equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"cost function","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transition time","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"trajectory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"propellant consumption","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"velocity","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"optimization","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":"Control of relative position change in formation flying","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Control of relative position change in formation flying","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":"7574","relation_version_is_last":true,"title":["Control of relative position change in formation flying"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:37:24.786606+00:00"}