{"created":"2023-06-20T15:14:09.737915+00:00","id":44135,"links":{},"metadata":{"_buckets":{"deposit":"3061c549-3fdd-408d-9ce6-2358965b4192"},"_deposit":{"created_by":1,"id":"44135","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"44135"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00044135","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["467894"],"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1986-05","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"106","bibliographicVolumeNumber":"552","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所資料"},{"bibliographic_title":"Technical Memorandum of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"科学技術庁航空宇宙技術研究所が研究開発を進めているファンジェットSTOL実験機には,機体の安定性と操縦性を高めるためにディジタル3重系自動飛行制御システム(SCAS)が搭載される。このSCASのセンサ系は,ポジションセンサ,慣性基準装置(IRU),IRUアダプタ,低速対気速度処理器,迎え角/横滑り角センサ,ディジタル対気諸元計算器,エンジン回転センサ(以上が新規開発機能部品)および全温度センサ,舵角センサから構成されている。ここでは新規開発センサの概要及び当該装備品がSTOL実験機に搭載可能であることを確認するために実施した認定試験の結果について記述する。","subitem_description_type":"Abstract"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTM0552000","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 TM-552","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":"0452-2982","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":"AN00314334","subitem_source_identifier_type":"NCID"}]},"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ＳＴＯＬプロジェクト推進本部実験機開発室操縦システム技術開発チーム"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"STOLプロジェクト推進本部実験機開発室操縦システム技術開発チーム"}],"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":"naltm00552.pdf","filesize":[{"value":"7.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00552.pdf","url":"https://jaxa.repo.nii.ac.jp/record/44135/files/naltm00552.pdf"},"version_id":"2892a5c1-ae12-4b15-8ae7-4dcd9b00f74d"}]},"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":"ファンジェットSTOL実験機自動飛行制御システム(SCAS)用センサの認定試験結果","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"ファンジェットSTOL実験機自動飛行制御システム(SCAS)用センサの認定試験結果"}]},"item_type_id":"3","owner":"1","path":["1893","1916"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"44135","relation_version_is_last":true,"title":["ファンジェットSTOL実験機自動飛行制御システム(SCAS)用センサの認定試験結果"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:02:01.930429+00:00"}