{"created":"2023-06-20T15:15:17.889322+00:00","id":45375,"links":{},"metadata":{"_buckets":{"deposit":"f9246702-9c2d-4545-bd4e-883a19370b6d"},"_deposit":{"created_by":1,"id":"45375","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"45375"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00045375","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["474417","474414","474418","474419","474415","474416"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Identification of the Stability and Control Derivatives of a DLC-Flap System for VSRA."}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1991-07","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"16","bibliographicVolumeNumber":"1116","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-1116","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"DLCフラップを装着した可変安定応答実験機(VSRA)のシステム・パラメータを知るために強制振動法による飛行実験を行った。水平定常飛行状態のトリムまわりで,DLCフラップを種々の周波数で持続的に加振し,その機体応答の周波数特性データからVSRAシステムの安定・操縦微係数を同定した。さらに,その操縦微係数からDLCフラップの揚力,抗力そして縦揺れモーメントを推定し,風洞試験結果とも比較した。その実験方法並びにデータ解析手法について述べる。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Flight tests were conducted using the Variable Stability and Response Airplane (VSRA) in order to identify the stability and control derivatives for a Direct Lift Control (DLC) flap system. The frequency response method was selected, with a pure sinusoidal input being applied to the DLC-flaps. Response from a linear system model consisting of the stability and control derivatives were compared with other flight test response data to determine general-inputs and resulting derivatives were subsequently verified. In addition, the control capability of the DLC-flaps was estimated by the control derivatives, and their compared with wind tunnel test data.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR1116000","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-1116","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飛行実験部"},{"subitem_text_value":"航空宇宙技術研究所飛行実験部"},{"subitem_text_value":"航空宇宙技術研究所飛行実験部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Flight Research Division, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Flight Research Division, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Flight Research Division, National Aerospace Laboratory(NAL)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"塚野, 雄吉"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小野, 孝次"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"石川, 和敏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"TSUKANO, Yukichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"ONO, Takatsugu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"ISHIKAWA, Kazutoshi","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":"naltr01116.pdf","filesize":[{"value":"1.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01116.pdf","url":"https://jaxa.repo.nii.ac.jp/record/45375/files/naltr01116.pdf"},"version_id":"8e8a98be-95ef-4f80-a7e5-bb4884ec59d3"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Stability/Control derivatives;  Flight Tests;  Frequency Response Method;  DLC-flaps;  In-flight simulator","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":"VSRA/DLCフラップ系の安定・操縦微係数の同定","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"VSRA/DLCフラップ系の安定・操縦微係数の同定"}]},"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":"45375","relation_version_is_last":true,"title":["VSRA/DLCフラップ系の安定・操縦微係数の同定"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:40:35.617596+00:00"}