{"created":"2023-06-20T15:15:17.798948+00:00","id":45373,"links":{},"metadata":{"_buckets":{"deposit":"33ccc0a0-1602-4937-8bbb-417a715c6ec4"},"_deposit":{"created_by":1,"id":"45373","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"45373"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00045373","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["474401","474402","474400","474398","474403","474405","474399","474404"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Damping Enhancement of Large Space Structures by Proof-Mass-Actuators"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1991-05","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"19","bibliographicVolumeNumber":"1114","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-1114","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"本論文は大型宇宙構造物LSSの構造減衰を能動的に増加する制御技術について述べる。このために,PMAとよばれるアクチュエータを設計・試作した。このPMAを使用して,構造減衰を達成するときの閉ループ系の安定条件をまず検討する。そして1入力1出力系,2入力2出力系の2つの場合の構造減衰の実験結果を示す。最後に,PMAのサイジングについて考察する。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The enhancement of modal damping is a key technology in Large Space Structures (LSS) robust control. A controller design is examined which augments substantial damping factors to LSS actively. The stability analysis of the closed-loop system is first discussed, being subsequently confirmed by a ground-based control experiment which used a newly developed pivoted type Proof Mass Actuator (PMA). The controller utilizes a direct velocity feedback control. A multi-input multi-output control system was examined using two PMAs, in addition to the single-input single-output case. In both cases, the experimental results showed excellent vibration suppression capability. A sizing problem of the PMAs is also discussed.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR1114000","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL TR-1114","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory(NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所宇宙研究グループ"},{"subitem_text_value":"航空宇宙技術研究所宇宙研究グループ"},{"subitem_text_value":"横浜国立大学"},{"subitem_text_value":"株式会社東芝"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Space Technology Research Group, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Space Technology Research Group, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Yokohama National University"},{"subitem_text_language":"en","subitem_text_value":"TOSHIBA Corporation"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"木田, 隆"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山口, 功"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"上野, 誠也"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"田中, 正樹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KIDA, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Isao, Yamaguchi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Seiya, Ueno","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Masaki, Tanaka","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-29"}],"displaytype":"detail","filename":"naltr01114.pdf","filesize":[{"value":"1.8 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01114.pdf","url":"https://jaxa.repo.nii.ac.jp/record/45373/files/naltr01114.pdf"},"version_id":"89bc8cf6-cae5-4e4d-8dbb-002959cecd1d"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"large space structures;  proof mass actuator;  robust stability;  vibrational 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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"PMAによる大型宇宙構造物の振動制御","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"PMAによる大型宇宙構造物の振動制御"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"45373","relation_version_is_last":true,"title":["PMAによる大型宇宙構造物の振動制御"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:40:37.572830+00:00"}