{"created":"2023-06-20T14:36:03.064157+00:00","id":2348,"links":{},"metadata":{"_buckets":{"deposit":"24565986-cb92-434f-b321-8f830fca3442"},"_deposit":{"created_by":1,"id":"2348","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2348"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002348","sets":["1887:1893","9:10:309:337"]},"author_link":["5549","5546","5552","5551","5548","5547","5550","5553"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Environmental testing technical report: Validation of force limit vibration testing using dummy satellite structure"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-03-28","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"JAXA-RR-04-030","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発報告"},{"bibliographic_title":"JAXA Research and Development Report","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"振動試験時の過大な加振力の入力による過負荷試験を避けるため、各国でフォースリミット制御の研究が行われている。宇宙航空研究開発機構(JAXA: Japan Aerospace Exploration Agency)試験センターでもフォースリミット制御の基礎研究を実施している。本論文では、いくつかのフォースリミット制御スペック計算方法について検討するとともに、性能評価用の供試体を作製して、JAXA試験センターの振動試験設備にてフォースリミット制御による振動試験の基礎実験を行った結果を報告する。","subitem_description_type":"Abstract"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0048139000","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-RR-04-030","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 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Center"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Tsukuba Space Center"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"長浜, 謙太"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shi, Qinzhong"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"安藤, 成将"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"三枝, 博"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nagahama, Kenta","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shi, Qinzhong","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ando, Shigemasa","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Saegusa, 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structure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"vibration test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"impedance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"resonant frequency","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"angular velocity","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"semiempirical equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"force limit 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 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