{"created":"2023-06-20T14:40:35.798294+00:00","id":7507,"links":{},"metadata":{"_buckets":{"deposit":"e9290f97-46c2-4e79-bc35-c2883992876d"},"_deposit":{"created_by":1,"id":"7507","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7507"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007507","sets":["1543:1544:1557","1887:1891"]},"author_link":["40049","40050"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"地球スイングバイを用いたソーラーセイルの最適軌道に関する研究"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2007-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"36","bibliographicPageStart":"32","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":"ソーラーセイルによる、地球フライバイ軌道の最適化に関する研究を行った。ソーラーセイルは近年実用化に向けて急速に開発が進んでいるが、とくに初期の応用段階においてはじゅうぶんな加速度を得るためにもフライバイを併用することが考えられる。本研究においては、最適制御理論および数値解析を用いて最適軌道を求め、セイル単独の場合と比べた場合の効率を考察した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Optimal trajectories for interplanetary mission with the combination of solar sail propulsion and Earth gravity assist are investigated. Solar sail is becoming a viable option for space exploration today, and the combination of gravity assist will be far effective to shorten the time of cruising phase, particularly on the initial stage of the application of solar sail propulsion. This article analyzes the trajectories with optimal control theory and the numerical simulations.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063481006","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 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 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":"花岡, 史紀"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hanaoka, Fuminori","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"ソーラーセイル","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道最適化","subitem_subject_scheme":"Other"},{"subitem_subject":"最適制御","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道計画","subitem_subject_scheme":"Other"},{"subitem_subject":"Pontryaginの原理","subitem_subject_scheme":"Other"},{"subitem_subject":"2体問題","subitem_subject_scheme":"Other"},{"subitem_subject":"Delta-VEGA","subitem_subject_scheme":"Other"},{"subitem_subject":"Delta-V","subitem_subject_scheme":"Other"},{"subitem_subject":"ヒルの方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"性能指数","subitem_subject_scheme":"Other"},{"subitem_subject":"加速度","subitem_subject_scheme":"Other"},{"subitem_subject":"スイングバイ技術","subitem_subject_scheme":"Other"},{"subitem_subject":"制御理論","subitem_subject_scheme":"Other"},{"subitem_subject":"数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"solar sail","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"trajectory optimization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"optimal control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"trajectory planning","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Pontryagin principle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"two body problem","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Delta-VEGA","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Delta-V","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Hill's equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"performance index","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"acceleration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"swingby technique","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"control theory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical analysis","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":"Optimal trajectories for EGA mission using solar sail","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Optimal trajectories for EGA mission using solar sail","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":"7507","relation_version_is_last":true,"title":["Optimal trajectories for EGA mission using solar sail"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:38:27.405169+00:00"}