{"created":"2023-06-20T14:41:03.886575+00:00","id":8097,"links":{},"metadata":{"_buckets":{"deposit":"0464714e-bb8f-40c9-8d3c-45e4d75ea01b"},"_deposit":{"created_by":1,"id":"8097","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"8097"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00008097","sets":["1543:1562:1577","1887:1891"]},"author_link":["44643","44638","44640","44639","44642","44641"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Attitude control for efficient improvement of Space Solar Power Satellite"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-06","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"56","bibliographicPageStart":"52","bibliographic_titles":[{"bibliographic_title":"第24回宇宙エネルギーシンポジウム　平成16年度"},{"bibliographic_title":"The Twenty-fourth Space Energy Symposium March 7, 2005","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper is devoted to analyze dynamical characteristics of a tethered Space Solar Power Satellite (SSPS) system proposed by the Japan Aerospace Exploration Agency (JAXA). The system consists of large, thin, flexible rectangle plates connected to a bus system through tethers. Attitude of the tethered SSPS is gravity-gradient stabilized with employment of tether technology. The control method is studied for the solar panel, which is directed toward solar light in order to improve the efficient generation of electric power. The controlled performance is analyzed by numerical simulation. The results show efficient performance of the tethered SSPS for the generation of sufficient electric power.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0049120011","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":"東京都立科学技術大学"},{"subitem_text_value":"東京都立科学技術大学"},{"subitem_text_value":"東京都立科学技術大学"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropolitan Institute of Technology"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropolitan Institute of Technology"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropolitan Institute of Technology"}]},"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":"古賀, 雄介"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"渡部, 武夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"藤井, 裕矩"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Koga, Yusuke","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Watanabe, Takeo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fujii, Hironori A.","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"宇宙太陽光利用システム","subitem_subject_scheme":"Other"},{"subitem_subject":"太陽発電衛星","subitem_subject_scheme":"Other"},{"subitem_subject":"テザー衛星","subitem_subject_scheme":"Other"},{"subitem_subject":"マイクロ波パワービーミング","subitem_subject_scheme":"Other"},{"subitem_subject":"レクテナ","subitem_subject_scheme":"Other"},{"subitem_subject":"静止軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星姿勢制御","subitem_subject_scheme":"Other"},{"subitem_subject":"太陽電池パネル","subitem_subject_scheme":"Other"},{"subitem_subject":"数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"運動方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"space solar power system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solar power satellite","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"tethered satellite","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"microwave power beaming","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rectenna","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"geostationary Earth orbit","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite attitude control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solar cell panel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"equation of motion","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"jpn"}]},"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":"テザー型宇宙太陽発電衛星の高効率化を目指したパネル姿勢制御","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"テザー型宇宙太陽発電衛星の高効率化を目指したパネル姿勢制御"}]},"item_type_id":"5","owner":"1","path":["1577","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"8097","relation_version_is_last":true,"title":["テザー型宇宙太陽発電衛星の高効率化を目指したパネル姿勢制御"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:28:32.114612+00:00"}