{"created":"2023-06-20T15:13:05.652399+00:00","id":42988,"links":{},"metadata":{"_buckets":{"deposit":"a662ff39-b065-414a-a5a0-29ac6dca9e38"},"_deposit":{"created_by":1,"id":"42988","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"42988"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00042988","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["461761","461756","461758","461757","461760","461755","461762","461759"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Airworthiness certification for MuPAL-alpha"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2003-07","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"775","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":"航空宇宙技術研究所では、ドルニエDo228-202型機を母機として、インフライト・シミュレーション機能を持つ多目的実証実験機MuPAL-αを開発した。MuPAL-αには、可変安定応答機能を実現するためにフライ・バイ・ワイヤ操縦装置や直接揚力制御装置を始めとする実験装置が装備され、様々な実験目的に合わせて飛行制御則やパイロットヘの飛行情報表示などを変更することができる。このような特徴を有する実験用航空機を安全かつできる限り通常の航空機と同様に運用するために、実験システム使用時も含めた耐空証明を取得した。本資料では、MuPAL-αが有する飛行形態と飛行モードを説明した後、実験用航空機としての汎用性と安全性を両立させるために工夫した点を中心に、各飛行形態に対する耐空性の証明について述べる。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The National Aerospace Laboratory of Japan (NAL) has modified a Dornier Do228-202 into an in-flight simulator, dubbed the MuPAL-alpha (Multi-Purpose Aviation Laboratory). The MuPAL-alpha is equipped with a Fly-By-Wire control system and a Direct Lift Control system, allowing variable stability and response capability. In the MuPAL-alpha, the flight control law and the format of the flight guidance display can be changed for each experiment task. To operate an experimental airplane with such features safely and in as similar manner as possible to ordinary aircraft, the NAL has obtained airworthiness certification for the MuPAL-alpha, including for the operation of experimental systems. This report first of all introduces the flight configurations and fight modes of the MuPAL-alpha, then discusses the policies and verification methods used to obtain the airworthiness certification, explaining the ideas that allow flexibility as an experimental airplane consistent with flight safety.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0047395000","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-775","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":"1347-460X","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 飛行システム研究センター"},{"subitem_text_value":"航空宇宙技術研究所 飛行システム研究センター"},{"subitem_text_value":"航空宇宙技術研究所 飛行システム研究センター"},{"subitem_text_value":"航空宇宙技術振興財団"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Flight Systems Research Center"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Flight Systems Research Center"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Flight Systems Research Center"},{"subitem_text_language":"en","subitem_text_value":"Foundation for Promotion of Japanese Aerospace Technology"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"増位, 和也"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"石川, 和敏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"稲垣, 敏治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"照井, 祐之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Masui, Kazuya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishikawa, Kazutoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Inagaki, Toshiharu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Terui, Yushi","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":"2020-01-28"}],"displaytype":"detail","filename":"naltm0000775.pdf","filesize":[{"value":"4.0 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm0000775.pdf","url":"https://jaxa.repo.nii.ac.jp/record/42988/files/naltm0000775.pdf"},"version_id":"90dc080f-0669-4895-8497-75e2e0830922"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"耐空性","subitem_subject_scheme":"Other"},{"subitem_subject":"航空機安定性","subitem_subject_scheme":"Other"},{"subitem_subject":"インフライト・シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"MuPal-α","subitem_subject_scheme":"Other"},{"subitem_subject":"可変安定性","subitem_subject_scheme":"Other"},{"subitem_subject":"フライ・バイ・ワイヤ制御","subitem_subject_scheme":"Other"},{"subitem_subject":"直接揚力制御","subitem_subject_scheme":"Other"},{"subitem_subject":"フライトモード","subitem_subject_scheme":"Other"},{"subitem_subject":"airworthiness","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aircraft stability","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"in-flight simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"MuPal-alpha","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"variable stability","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"fly by wire control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"direct lift control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight mode","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":"多目的実証実験機MuPAL-αの耐空性の証明","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"多目的実証実験機MuPAL-αの耐空性の証明"}]},"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":"42988","relation_version_is_last":true,"title":["多目的実証実験機MuPAL-αの耐空性の証明"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:22:37.518316+00:00"}