{"created":"2023-06-20T15:10:17.143871+00:00","id":39873,"links":{},"metadata":{"_buckets":{"deposit":"5e1c5f8a-03d7-43f2-a173-a1cf60415e8d"},"_deposit":{"created_by":1,"id":"39873","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"39873"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00039873","sets":["1887:1893","1896:1898:1933:1934"]},"author_link":["500833","500832","500841","500839","500836","500838","500831","500843","500834","500830","500837","500840","500835","500842"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Evaluation of six DoF active vibration isolation system under microgrvity condition, no. 3"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1997-01-31","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"10","bibliographicPageStart":"1","bibliographic_titles":[{"bibliographic_title":"宇宙開発事業団技術報告"},{"bibliographic_title":"NASDA Technical Memorandum","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"微小重力環境下での加速度外乱を低減させるため、能動制振システムを開発してきた。MU-300型航空機を使用して行った第3回微小重力実験で、本システムの制振性能評価を行った。ここでデジタル演算制御を新たに制御システムに採用した。2種の制御法である相対変位フィードバック制御と加速度フィードバック制御もあわせて試験した。実験結果から、航空機による微小重力中の振動外乱は、能動制振システムを使い顕著に低減することが明らかとなった。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"An active vibration isolation system has been developing to reduce accelerational disturbances in microgravity environment. The third microgravity experiment using MU-300 type aircraft was conducted to evaluate the vibration isolation performance of the system. The digital operation was newly applied to the control system. Two kinds of control methods were also examined, namely relative displacement feedback control and acceleration feedback control. It became clear from the experimental results that vibrational disturbances in the aircraft-generated microgravity were remarkably reduced by using the active vibration isolation system.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000789001","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: NASDA-TMR-960027","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙開発事業団"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Space Development Agency of Japan (NASDA)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1345-7888","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00364784","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙開発事業団"},{"subitem_text_value":"宇宙開発事業団"},{"subitem_text_value":"宇宙環境利用推進センター"},{"subitem_text_value":"石川島播磨重工業"},{"subitem_text_value":"石川島播磨重工業"},{"subitem_text_value":"石川島防音工業"},{"subitem_text_value":"石川島播磨重工業"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Space Development Agency of Japan"},{"subitem_text_language":"en","subitem_text_value":"National Space Development Agency of Japan"},{"subitem_text_language":"en","subitem_text_value":"Japan Space Utilization Promotion Center"},{"subitem_text_language":"en","subitem_text_value":"Ishikawajima-Harima Heavy Industries Co Ltd"},{"subitem_text_language":"en","subitem_text_value":"Ishikawajima-Harima Heavy Industries Co Ltd"},{"subitem_text_language":"en","subitem_text_value":"Ishikawajima Noise Control Co Ltd"},{"subitem_text_language":"en","subitem_text_value":"Ishikawajima-Harima Heavy Industries Co Ltd"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"依田, 真一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"石井, 誠一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小西, 貴明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"星, 聖子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"鈴木, 寿幸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"大久保, 孝一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"桑原, 啓一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yoda, Shinichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishii, Seiichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Konishi, Takaharu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hoshi, Seiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Suzuki, Yasuyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Okubo, Koichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kuwabara, Keiichi","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":"2020-02-10"}],"displaytype":"detail","filename":"00789001.pdf","filesize":[{"value":"664.0 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"00789001.pdf","url":"https://jaxa.repo.nii.ac.jp/record/39873/files/00789001.pdf"},"version_id":"65332603-716e-4533-9903-f39562bd97ff"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"MU-300型航空機","subitem_subject_scheme":"Other"},{"subitem_subject":"パラボリックフライト","subitem_subject_scheme":"Other"},{"subitem_subject":"微小重力環境","subitem_subject_scheme":"Other"},{"subitem_subject":"能動制振システム","subitem_subject_scheme":"Other"},{"subitem_subject":"加速度外乱","subitem_subject_scheme":"Other"},{"subitem_subject":"振動遮断性能","subitem_subject_scheme":"Other"},{"subitem_subject":"振動外乱低減","subitem_subject_scheme":"Other"},{"subitem_subject":"デジタル演算制御","subitem_subject_scheme":"Other"},{"subitem_subject":"相対変位フィードバック制御","subitem_subject_scheme":"Other"},{"subitem_subject":"加速度フィードバック制御","subitem_subject_scheme":"Other"},{"subitem_subject":"非線形懸架ばね","subitem_subject_scheme":"Other"},{"subitem_subject":"MU 300 aircraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"parabolic flight","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"microgravity environment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"active vibration isolation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"accelerational disturbance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"vibration isolation ability","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"vibrational disturbance reduction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"digital operation control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"relative displacement feedback control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"acceleration feedback control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"nonlinear suspension spring","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":"航空機による微小重力実験:6自由度能動制振システム機能・性能評価試験　その3","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"航空機による微小重力実験:6自由度能動制振システム機能・性能評価試験　その3"}]},"item_type_id":"3","owner":"1","path":["1893","1934"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"39873","relation_version_is_last":true,"title":["航空機による微小重力実験:6自由度能動制振システム機能・性能評価試験　その3"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T20:28:23.041994+00:00"}