{"created":"2023-06-20T14:39:18.998211+00:00","id":6054,"links":{},"metadata":{"_buckets":{"deposit":"909e6ce3-0bcd-4214-8ce8-09c43a44b6c0"},"_deposit":{"created_by":1,"id":"6054","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6054"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006054","sets":["1887:1893","9:789:998:1028"]},"author_link":["30173","30172","30171","30169","30170","30175","30174","30176"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Measurement technology of micro-vibration transmission: Researches on space structural technology"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2006-11-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"329","bibliographicPageStart":"325","bibliographicVolumeNumber":"JAXA-SP-06-006","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 平成18年度　宇宙航空研究開発機構　総合技術研究本部　宇宙科学研究本部　研究成果報告書"},{"bibliographic_title":"JAXA Special Publication: Report on Research Achievements for FY2006 Institute of Space and Astronautical Science, Institute of Aerospace Technology, Japan Aerospace Exploration Agency","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Pointing Accuracy of sensors and stability of attitude control of spacecraft are influenced by micro-vibration transmitted from components, for example, reaction wheels and coolers, which are regarded as internal disturbance sources. Such micro-vibration should be controlled and managed on early design phase. In order to establish the control method, characteristics of the micro-vibration transmissibility have to be measured and evaluated. Thus, the measurement and testing methods of the micro-vibration are investigated.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0049500070","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: JAXA-SP-06-006","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","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":"AA11984031","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 宇宙科学研究本部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Aerospace Technology"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Aerospace Technology"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Aerospace Technology"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"内田, 英樹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"清水, 隆三"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"遠藤, 達也"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小松, 敬治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Uchida, Hideki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shimizu, Ryuzo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Endo, Tatsuya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Komatsu, Keiji","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":"2020-01-16"}],"displaytype":"detail","filename":"49500070.pdf","filesize":[{"value":"893.7 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"49500070.pdf","url":"https://jaxa.repo.nii.ac.jp/record/6054/files/49500070.pdf"},"version_id":"76b97bce-0d99-41ac-9f22-c86004adb029"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"振動測定","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機部品","subitem_subject_scheme":"Other"},{"subitem_subject":"振動伝達","subitem_subject_scheme":"Other"},{"subitem_subject":"振動減衰","subitem_subject_scheme":"Other"},{"subitem_subject":"振動試験","subitem_subject_scheme":"Other"},{"subitem_subject":"内部擾乱","subitem_subject_scheme":"Other"},{"subitem_subject":"加速計","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星姿勢制御","subitem_subject_scheme":"Other"},{"subitem_subject":"vibration measurement","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft component","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"vibration transmission","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"vibration damping","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"vibration test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"internal disturbance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"accelerometer","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite 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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"擾乱伝達計測技術の研究:構造技術の研究","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"擾乱伝達計測技術の研究:構造技術の研究"}]},"item_type_id":"3","owner":"1","path":["1028","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"6054","relation_version_is_last":true,"title":["擾乱伝達計測技術の研究:構造技術の研究"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:03:06.734186+00:00"}