{"created":"2023-06-20T15:14:10.161525+00:00","id":44141,"links":{},"metadata":{"_buckets":{"deposit":"dc614b38-1082-48d4-b2bb-0d7b2e18c0ba"},"_deposit":{"created_by":1,"id":"44141","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"44141"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00044141","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["467945","467946"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Basic Desing of a Flight Directer System for NAL STOL Research Aircraft"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1986-12","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"24","bibliographicVolumeNumber":"558","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_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A basic design concept of a flight director system for the NAL STOL Research Air-craft “ASUKA” is proposed and evaluated with the help of a CAD (Computer Aided Design) tool for control system synthesis. The flight director system designed for backside operations during the approach and landing phase of ASUKA has three commands presented by one integrated symbol : pitch command for speed control, flight path command for Flight Path Control lever manipulation, and bank command for lateral control. In determining the flight-director dynamics, closed loop analysis was conducted of pilot, aircraft, control systems, and navigational sites, as well as the flight director system itself. Dialogical communications with the CAD system enabled the quick and simple determination of the dynamics. Dynamics and constants of the flight director system confirmed by the present study form a basis for future design of flight director systems for USB type aircraft.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTM0558000","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-558","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飛行実験部"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"田中, 敬司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"TANAKA, 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":"2020-01-29"}],"displaytype":"detail","filename":"naltm00558.pdf","filesize":[{"value":"1.3 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00558.pdf","url":"https://jaxa.repo.nii.ac.jp/record/44141/files/naltm00558.pdf"},"version_id":"47b40c2e-82ad-41a3-9fd7-3dba4ec3f9f2"}]},"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":"STOL実験機用フライト・ディレクタ・システムの基礎設計","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"STOL実験機用フライト・ディレクタ・システムの基礎設計"}]},"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":"44141","relation_version_is_last":true,"title":["STOL実験機用フライト・ディレクタ・システムの基礎設計"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:01:57.420634+00:00"}