{"created":"2023-06-20T15:11:27.843262+00:00","id":41125,"links":{},"metadata":{"_buckets":{"deposit":"106af75b-346b-4929-93af-fb57a1f2b821"},"_deposit":{"created_by":1,"id":"41125","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41125"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041125","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["450634","450635"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Flight test evaluations of the head-up display and the inertial reference unit of the NAL QSTOL experimental aircraft (Aska) by the NAL B-65 Queen Air research aircraft"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1993-07","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"47","bibliographicPageStart":"1","bibliographicVolumeNumber":"658","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":"本稿は、ファンジェットSTOL(短距離離着陸)実験機(飛鳥)用に開発されたHUD(ヘッドアップディスプレイ)およびIRU(慣性基準装置)を航空宇宙技術研究所(NAL)所有のビーチクラフト65型クインエア実験用航空機に搭載して、HUDの有効性、ならびにIRUを飛行制御、計測のセンサとして用いるための精度、特性を評価するために行った飛行評価試験についてまとめたものである。この評価試験を通じて確認されたことは以下の通りである。(1)HUDが着陸時の飛行援助装置として有効である。(2)HUDが飛行試験の遂行においても有効である。(3)IRUは実環境下において認定基準を満足する性能を有する。また、今後の新しい航空機へのHUD、IRUの適用面においては、以下の点で有用なデータを提供した。(4)HUDを搭載する航空機のための基本的な飛行試験技術を確立した。(5)IRUの実機搭載による性能評価法を確立した。(6)レーダガイダンスなどと組み合わせたHUDによる新しい計器着陸技術の可能性を明らかにした。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A Head-Up Display (HUD) and an Inertial Reference Unit (IRU) were developed by the National Aerospace Laboratory (NAL) for the NAL QSTOL (Quiet Short Take Off and Landing) experimental aircraft (Aska). Flight tests were conducted in the B-65 Queen Air, and the performance of the HUD which provides the pilot with landing aid information, and the accuracy and characteristics of the IRU to be used for flight control and measurements were evaluated. The results indicated that the HUD accuracy and characteristics of the HUD as an approach and landing aid system were good, and also that the IRU was useful as a sensor for flight control and measurements. Furthermore, methods of evaluating HUD characteristics and IRU accuracy in-flight are discussed.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004146000","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-658","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"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"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"}],"nameIdentifiers":[{"nameIdentifier":"450634","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"STOL Research Aircraft Group","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"450635","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":"2020-01-27"}],"displaytype":"detail","filename":"naltm00658.pdf","filesize":[{"value":"4.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00658.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41125/files/naltm00658.pdf"},"version_id":"c94cafab-99f6-4aa6-90bf-d1d4cf7ccb82"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"ヘッドアップディスプレイ","subitem_subject_scheme":"Other"},{"subitem_subject":"慣性基準装置","subitem_subject_scheme":"Other"},{"subitem_subject":"ストラップダウン慣性航法装置","subitem_subject_scheme":"Other"},{"subitem_subject":"ILS","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行試験","subitem_subject_scheme":"Other"},{"subitem_subject":"計器着陸システム","subitem_subject_scheme":"Other"},{"subitem_subject":"分解能","subitem_subject_scheme":"Other"},{"subitem_subject":"測定精度","subitem_subject_scheme":"Other"},{"subitem_subject":"位置測定","subitem_subject_scheme":"Other"},{"subitem_subject":"レーダガイダンス","subitem_subject_scheme":"Other"},{"subitem_subject":"方位角","subitem_subject_scheme":"Other"},{"subitem_subject":"キャリブレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"STOL機","subitem_subject_scheme":"Other"},{"subitem_subject":"飛鳥","subitem_subject_scheme":"Other"},{"subitem_subject":"騒音抑制","subitem_subject_scheme":"Other"},{"subitem_subject":"headup display","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"inertial reference unit","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"strapdown inertial navigation system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Instrument Landing System","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ILS","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"resolving power","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"measurement accuracy","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"position measurement","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"radar guidance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"azimuth angle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"calibration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"STOL aircraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Aska","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"noise 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 report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"低騒音STOL実験機用HUD(ヘッドアップディスプレイ)及びIRU(慣性基準装置)の飛行評価試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"低騒音STOL実験機用HUD(ヘッドアップディスプレイ)及びIRU(慣性基準装置)の飛行評価試験"}]},"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":"41125","relation_version_is_last":true,"title":["低騒音STOL実験機用HUD(ヘッドアップディスプレイ)及びIRU(慣性基準装置)の飛行評価試験"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:13:37.098383+00:00"}