{"created":"2023-06-20T14:40:43.363313+00:00","id":7643,"links":{},"metadata":{"_buckets":{"deposit":"bc8ae249-7910-4dc9-8ee7-7e82c3fe52a6"},"_deposit":{"created_by":1,"id":"7643","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7643"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007643","sets":["1543:1544:1559","1887:1891"]},"author_link":["40940","40941","40944","40946","40948","40943","40942","40947","40939","40949","40950","40945"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"スピンフォーメーション・ソーラーセールの膜面展開"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"60","bibliographicPageStart":"55","bibliographic_titles":[{"bibliographic_title":"平成16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 14th Workshop on Astrodynamics and Flight Mechanics 2004: A Collection of Technical Papers","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In the paper, a new type membrane deployment method is proposed, and locally full-deployment state can be achieved in the deployment from folded state. Fundamental ground experiments of the proposed membrane deployment are conducted using an experimental set-up system including two-dimensional micro-gravity simulators, and tether and membrane control mechanisms developed at Tokyo Institute of Technology. The simulator system is composed of a 3 m x 5 m flat-floor glass and floating satellite simulators with gas-thruster. Here, used are three satellite simulators, triangular membranes, the tether control system and newly developed drum mechanisms for membrane control. The drum mechanism can control membrane extension speed. A virtual structure control method is applied to control the three satellites for formation flight, and PID type control is adopted to control the membrane control. From the experiment obtained is two-dimentional deployment behavior and the feasibility of the proposed method is discussed comparing with corresponding numerical simulation results.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0047897010","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_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":"東京工業大学 大学院理工学研究科"},{"subitem_text_value":"東京工業大学 大学院理工学研究科"},{"subitem_text_value":"東京工業大学 大学院理工学研究科"},{"subitem_text_value":"東京工業大学 大学院理工学研究科"},{"subitem_text_value":"東京工業大学 大学院理工学研究科"},{"subitem_text_value":"東京工業大学 大学院理工学研究科"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Tokyo Institute of Technology Graduate School of Science and Engineering"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Institute of Technology Graduate School of Science and Engineering"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Institute of Technology Graduate School of Science and Engineering"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Institute of Technology Graduate School of Science and Engineering"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Institute of Technology Graduate School of Science and Engineering"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Institute of Technology Graduate School of Science and 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":"松永, 三郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"矢部, 秀幸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中谷, 幸司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"居相, 政史"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"尾曲, 邦之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"森, 治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsunaga, Saburo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yabe, Hideyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakaya, Koji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Iai, Masafumi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Omagari, Kuniyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Mori, Osamu","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"膜面展開","subitem_subject_scheme":"Other"},{"subitem_subject":"編成飛行","subitem_subject_scheme":"Other"},{"subitem_subject":"ソーラーセール","subitem_subject_scheme":"Other"},{"subitem_subject":"微小重力","subitem_subject_scheme":"Other"},{"subitem_subject":"数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"人工衛星","subitem_subject_scheme":"Other"},{"subitem_subject":"予備調査","subitem_subject_scheme":"Other"},{"subitem_subject":"membrane deployment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"formation flight","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solar sail","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"microgravity","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"artificial satellite","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"feasibility study","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":"Membrane deployment for spinning formation-flight solar sail","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Membrane deployment for spinning formation-flight solar sail","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1559","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7643","relation_version_is_last":true,"title":["Membrane deployment for spinning formation-flight solar sail"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:36:18.755068+00:00"}