{"created":"2023-06-20T14:53:40.099676+00:00","id":21895,"links":{},"metadata":{"_buckets":{"deposit":"36ecf25f-0114-4b6a-8626-414e695a3649"},"_deposit":{"created_by":1,"id":"21895","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"21895"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00021895","sets":["1887:1888"]},"author_link":["205107","205102","205105","205104","205106","205103"],"item_7_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"System Identification for Large Flexible Spacecraft Using Accelerometers : Iterative Algorithm for Mode Model Ideitification"}]},"item_7_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2008","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"6","bibliographicPageEnd":"524","bibliographicPageStart":"518","bibliographicVolumeNumber":"44","bibliographic_titles":[{"bibliographic_title":"計測自動制御学会論文集"}]}]},"item_7_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: PA0810081000","subitem_description_type":"Other"}]},"item_7_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"計測自動制御学会"}]},"item_7_relation_25":{"attribute_name":"DOI","attribute_value_mlt":[{"subitem_relation_name":[{"subitem_relation_name_text":"info:doi/10.9746/ve.sicetr1965.44.518"}],"subitem_relation_type_id":{"subitem_relation_type_id_text":"http://dx.doi.org/10.9746/ve.sicetr1965.44.518","subitem_relation_type_select":"DOI"}}]},"item_7_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0453-4654","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":"AN00072392","subitem_source_identifier_type":"NCID"}]},"item_7_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構研究開発本部構造･機構ｸﾞﾙｰﾌﾟ (JAXA)(ARD)"},{"subitem_text_value":"宇宙航空研究開発機構研究開発本部構造･機構ｸﾞﾙｰﾌﾟ (JAXA)(ARD)"},{"subitem_text_value":"宇宙航空研究開発機構研究開発本部構造･機構ｸﾞﾙｰﾌﾟ (JAXA)(ARD)"}]},"item_7_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency, Aerospace Research and Development Directorate (JAXA)(ARD)"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency, Aerospace Research and Development Directorate (JAXA)(ARD)"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency, Aerospace Research and Development Directorate (JAXA)(ARD)"}]},"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":"山口, 功"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"葛西, 時雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"井川, 寛隆"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"YAMAGUCHI, Isao","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KASAI, Tokio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"IGAWA, Hirotaka","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"SIMO","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"system ideitification","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"large flexible spacecraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"accelerometers","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"iterative algorithm","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":"加速度計出力を用いた柔軟構造衛星のシステム同定 : インパルス加振によるモードモデルの回帰的同定","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"加速度計出力を用いた柔軟構造衛星のシステム同定 : インパルス加振によるモードモデルの回帰的同定"}]},"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":"21895","relation_version_is_last":true,"title":["加速度計出力を用いた柔軟構造衛星のシステム同定 : インパルス加振によるモードモデルの回帰的同定"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T03:29:16.851060+00:00"}