{"created":"2023-06-20T14:40:47.851949+00:00","id":7739,"links":{},"metadata":{"_buckets":{"deposit":"607c3a77-bf87-4a83-8cc0-787131155472"},"_deposit":{"created_by":1,"id":"7739","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7739"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007739","sets":["1543:1544:1560","1887:1891"]},"author_link":["41591","41596","41595","41593","41598","41597","41592","41594","41600","41599"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"テザー太陽発電衛星の姿勢制御に関する数値解析"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2004-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"244","bibliographicPageStart":"239","bibliographic_titles":[{"bibliographic_title":"平成15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 13th Workshop on Astrodynamics and Flight Mechanics 2003: A Collection of Technical Papers","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"無人宇宙実験システム研究開発機構(USEF)の提案する、テザー太陽発電衛星(SSPS)について、その姿勢運動を制御するアルゴリズムについての研究を行った。姿勢運動に関する可制御性は、SSPSによって発生したエネルギーを地上に送るために不可欠な技術要素のひとつである。このSSPSは、矩形の発送電一体型パネルの4隅から伸びたテザーがバス部につながっており、重力傾度トルクによって受動的に安定性を得る構造となっている。このバス部をテザー長の変化によって動かすことでシステムの慣性能率を変化させることにより姿勢制御を行う。数値解析の結果、ピッチ方向の運動に加えて、ロールヨー方向においても、基本的な応答特性などの知見を得た。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Control algorithm is studied for the attitude motion of a tethered Space Solar Power Satellite (SSPS). Controllability of the attitude motion of the system is essential for the SSPS to accomplish the mission to collect solar power and deliver to the surface of the Earth. The SSPS is a rectangular solar panel connected a bus unit by four tethers to stabilize the system passively by use of the gravity gradient effect. The attitude motion is proposed to be controlled by a mass moving its position with respect to the solar panel through change of the length of tethers. Numerical simulator is constructed in order to implement the control algorithms to verify the validity of performances of the present control methods.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0046652038","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":"東京都立科学技術大学 工学部　航空宇宙システム工学科"},{"subitem_text_value":"東京都立科学技術大学 大学院工学研究科"},{"subitem_text_value":"東京都立科学技術大学 工学部　航空宇宙システム工学科"},{"subitem_text_value":"東京都立科学技術大学 大学院工学研究科"},{"subitem_text_value":"東京都立科学技術大学 大学院工学研究科"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropolitan Institute of Technology Department of Aerospace Engineering, Faculty of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropolitan Institute of Technology Graduate School of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropolitan Institute of Technology Department of Aerospace Engineering, Faculty of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropolitan Institute of Technology Graduate School of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropolitan Institute of Technology Graduate 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":"藤井, 裕矩"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"渡部, 武夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小島, 広久"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"関川, 和馬"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小林, 直樹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fujii, Hironori A.","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Watanabe, Takeo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kojima, Hirohisa","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sekikawa, Kazuma","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kobayashi, Naoki","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"SSPS","subitem_subject_scheme":"Other"},{"subitem_subject":"数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"姿勢制御","subitem_subject_scheme":"Other"},{"subitem_subject":"太陽発電機","subitem_subject_scheme":"Other"},{"subitem_subject":"制御性","subitem_subject_scheme":"Other"},{"subitem_subject":"テザーリング","subitem_subject_scheme":"Other"},{"subitem_subject":"重力勾配","subitem_subject_scheme":"Other"},{"subitem_subject":"アルゴリズム","subitem_subject_scheme":"Other"},{"subitem_subject":"SSPS","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"attitude control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solar generator","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"controllability","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"tethering","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"gravity gradient","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"algorithm","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":"Numerical analysis of the attitude control of a tethered Space Solar Power Satellite","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Numerical analysis of the attitude control of a tethered Space Solar Power Satellite","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1560","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7739","relation_version_is_last":true,"title":["Numerical analysis of the attitude control of a tethered Space Solar Power Satellite"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:34:48.359921+00:00"}