{"created":"2023-06-20T14:59:19.876413+00:00","id":28224,"links":{},"metadata":{"_buckets":{"deposit":"4482e8fd-be24-4ad1-9d20-d87fd1ca3819"},"_deposit":{"created_by":1,"id":"28224","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"28224"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00028224","sets":["1887:1888"]},"author_link":["342057","342059","342060","342058"],"item_7_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Design and Hardware Verification of Canard Based Sounding Rocket Attitude Controller Using Adaptive Filter"}]},"item_7_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2002","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"10","bibliographicPageStart":"1","bibliographicVolumeNumber":"1","bibliographic_titles":[{"bibliographic_title":"宇宙技術"},{"bibliographic_title":"Space Technology Japan","bibliographic_titleLang":"en"}]}]},"item_7_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA1004932000","subitem_description_type":"Other"}]},"item_7_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"日本航空宇宙学会"}]},"item_7_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"The Japan Society of Aeronautical and Space Sciences"}]},"item_7_relation_25":{"attribute_name":"DOI","attribute_value_mlt":[{"subitem_relation_name":[{"subitem_relation_name_text":"info:doi/10.2322/stj.1.1"}],"subitem_relation_type_id":{"subitem_relation_type_id_text":"http://dx.doi.org/10.2322/stj.1.1","subitem_relation_type_select":"DOI"}}]},"item_7_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1347-3832","subitem_source_identifier_type":"ISSN"}]},"item_7_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙科学研究所 (ISAS)"},{"subitem_text_value":"（株）アイ・エイチ・アイ・エアロスペース"}]},"item_7_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Astronautical Science (ISAS)"},{"subitem_text_language":"en","subitem_text_value":"IHI AEROSPACE Co., Ltd."}]},"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":"澤井, 秀次郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松田, 聖路"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sawai, Shujiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsuda, Seiji","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Rockets","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Attitude Control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Canard","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Adaptive 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":"動翼を用いた観測ロケットの適応型姿勢制御系の設計とハードウェア試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"動翼を用いた観測ロケットの適応型姿勢制御系の設計とハードウェア試験"}]},"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":"28224","relation_version_is_last":true,"title":["動翼を用いた観測ロケットの適応型姿勢制御系の設計とハードウェア試験"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T01:53:06.406828+00:00"}