{"created":"2023-06-20T14:54:12.355840+00:00","id":22487,"links":{},"metadata":{"_buckets":{"deposit":"36d8377b-62d8-4509-a25e-dd8f572fb881"},"_deposit":{"created_by":1,"id":"22487","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"22487"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00022487","sets":["1887:1888"]},"author_link":["210876","210883","210877","210885","210878","210879","210881","210884","210880","210882"],"item_7_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Robust Attitude Control of Large Flexible Spacecraft: Application of Input Constrained Model Predictive Control"}]},"item_7_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2013-06-25","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"802","bibliographicPageEnd":"1948","bibliographicPageStart":"1935","bibliographicVolumeNumber":"79","bibliographic_titles":[{"bibliographic_title":"日本機械学会論文集Ｃ編"},{"bibliographic_title":"Transactions of the Japan Society of Mechanical Engineers. C","bibliographic_titleLang":"en"}]}]},"item_7_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper presents an application of the model predictive control to flexible spacecraft attitude maneuver. The objective of the study is to demonstrate an experimental feasibility of optimal attitude controllers suppressing the flexible appendage vibration under the actuator saturation. For the purpose, we study two approaches in the model predictive control framework. One is to use the frequency-shaped linear quadratic cost with finite horizon, and the other is to apply the robust control theory. Through ground experiments using a single axis air bearing table, as well as numerical studies for ETS-VIII spacecraft, their abilities are shown and compared.","subitem_description_type":"Other"}]},"item_7_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: PA1420038000","subitem_description_type":"Other"}]},"item_7_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"日本機械学会(JSME)"}]},"item_7_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"The Japan Society of Mechanical Engineers (JSME)"}]},"item_7_relation_25":{"attribute_name":"DOI","attribute_value_mlt":[{"subitem_relation_name":[{"subitem_relation_name_text":"info:doi/10.1299/kikaic.79.1935"}],"subitem_relation_type_id":{"subitem_relation_type_id_text":"http://dx.doi.org/10.1299/kikaic.79.1935","subitem_relation_type_select":"DOI"}}]},"item_7_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0387-5024","subitem_source_identifier_type":"ISSN"}]},"item_7_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00187463","subitem_source_identifier_type":"NCID"},{"subitem_source_identifier":"AA11553029","subitem_source_identifier_type":"NCID"}]},"item_7_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"電気通信大学"},{"subitem_text_value":"宇宙航空研究開発機構研究開発本部(JAXA)"},{"subitem_text_value":"防衛大学校"},{"subitem_text_value":"大阪府立大学"},{"subitem_text_value":"電気通信大学"}]},"item_7_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"The University of Electro-Communications (UEC)"},{"subitem_text_language":"en","subitem_text_value":"Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"National Defense Academy of Japan (NDA)"},{"subitem_text_language":"en","subitem_text_value":"Osaka Prefecture University"},{"subitem_text_language":"en","subitem_text_value":"The University of Electro-Communications (UEC)"}]},"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":"山下, 哲生"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"濱田, 吉郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山口, 功"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"長塩, 知之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"木田, 隆"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamashita, Tetsuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hamada, Yoshiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamaguchi, Isao","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nagashio, Tomoyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kida, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Model Predictive Control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Robust Control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Input-Constraint","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Flexible Spacecraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Attitude Control","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":"journal article","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"大型柔軟衛星のロバスト姿勢制御（入力拘束を考慮したモデル予測制御の適用）","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"大型柔軟衛星のロバスト姿勢制御（入力拘束を考慮したモデル予測制御の適用）"}]},"item_type_id":"7","owner":"1","path":["1888"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"22487","relation_version_is_last":true,"title":["大型柔軟衛星のロバスト姿勢制御（入力拘束を考慮したモデル予測制御の適用）"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T03:20:20.779259+00:00"}