{"created":"2023-06-20T15:14:09.879262+00:00","id":44137,"links":{},"metadata":{"_buckets":{"deposit":"1dee210c-6d56-4867-9b22-8562f8ca2e00"},"_deposit":{"created_by":1,"id":"44137","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"44137"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00044137","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["467910","467908","467909","467907"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"The First Flight Simulator Test of the Head-Up Display for NAL QSTOL Experimental Aircraft (ASUKA)"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1986-10","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"32","bibliographicVolumeNumber":"554","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 head-up display (HUD), which was designed by the National Aerospace Laboratory (NAL) and manufactured for the NAL QSTOL (Quiet Short Take-Off and Landing) experimental aircraft, Asuka, also developed by NAL, was evaluated with the STOL flight simulator. The unprecedented feature of this HUD is that it provides the aircraft with the ability to perform in-flight approach and flare simulation. The flight simulator evaluation was conducted to verify functions of the six display modes: Basic, Normal, Velocity-Vector, Pseudo-approach-type-A (ILS deviation format), Pseudo-approach-type-B (flight-path error format), and Pseudo-approach-type-C (flight director format), and to obtain data for improving performance of the HUD. About 400 simulated approach-and-landing flights evaluated by four test pilots revealed that the HUD has significant effect in improving approach performance and reducing pilot workload, and that the HUD’s inflight approach function is satisfactory for the QSTOL. Also, suggestions to impro the display format of each display mode were obtained.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTM0554000","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-554","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開発室"},{"subitem_text_value":"航空宇宙技術研究所操縦システム開発チーム"},{"subitem_text_value":"航空宇宙技術研究所飛行解析チーム"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Development Section"}]},"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開発室"}],"nameIdentifiers":[{"nameIdentifier":"467907","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"操縦システム開発チーム"}],"nameIdentifiers":[{"nameIdentifier":"467908","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"飛行解析チーム"}],"nameIdentifiers":[{"nameIdentifier":"467909","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Development Section","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"467910","nameIdentifierScheme":"WEKO"}]}]},"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":"naltm00554.pdf","filesize":[{"value":"3.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00554.pdf","url":"https://jaxa.repo.nii.ac.jp/record/44137/files/naltm00554.pdf"},"version_id":"f051c99d-dc44-4f50-b5c4-bbbd00e6654d"}]},"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":"低騒音STOL実験機(飛鳥)用HUD(ヘッド・アップ・ディスプレイ)の第一次シミュレーション評価試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"低騒音STOL実験機(飛鳥)用HUD(ヘッド・アップ・ディスプレイ)の第一次シミュレーション評価試験"}]},"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":"44137","relation_version_is_last":true,"title":["低騒音STOL実験機(飛鳥)用HUD(ヘッド・アップ・ディスプレイ)の第一次シミュレーション評価試験"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:34:14.985598+00:00"}