{"created":"2023-06-20T15:07:50.567089+00:00","id":37206,"links":{},"metadata":{"_buckets":{"deposit":"f8a12d28-9da0-41bd-82db-d0373004dafa"},"_deposit":{"created_by":1,"id":"37206","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37206"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037206","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["479551","479549","479546","479545","479552","479554","479555","479557","479548","479553","479561","479558","479547","479544","479559","479556","479550","479560"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"小型自動着陸実験(ALFLEX)機の開発"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1998-08","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"26","bibliographicPageStart":"17","bibliographicVolumeNumber":"39T","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"航空宇宙技術研究所　宇宙開発事業団 28 Feb. 1997 Sydney","subitem_description_type":"Other"}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"National Aerospace Laboratory. National Space Development Agency of Japan 28 Feb. 1997 Sydney Australia","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"自動着陸技術は日本製スペースシャトル「HOPE」に必要な基盤技術の一つである。自動着陸実験機(ALFLEX)は無人型で、HOPEの37%模型であり、完全自動着陸の基礎を確立するために使われている。ALFLEXの構造はHOPEのベースラインを動力学的に模擬しており、その飛行プロフィールは着陸段階だけを仮定している。通常のアルミ合金が機体の主構造を形成しており、二重湾曲のスキンパネルには繊維強化プラスチックも用いた。機体は完全に独立した自動着陸用の電気系統を装備しており、地上の安全性のために緊急システムも備えている。製作に要する時間と費用を節約するために、既製のデバイス類を用いた。実験の結果、自動着陸技術を無人機へ使用することは適していることを確認した。このサブスケール模型を使用して、低速空力特性を含む重要な飛行データを得た。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"An automatic landing technology is one of the key technologies necessary for the Japanese Space Shuttle 'HOPE' (H-2 Orbiting Plane). The ALFLEX (Automatic Landing Flight Experiment) vehicle is an unmanned, 37 percent scaled model of HOPE (H-2 Orbiting Plane), which is used to establish the fundamentals for fully automatic landing. The configuration of ALFLEX is simulating dynamically a HOPE baseline and its flight profile assumes only the landing phase. Conventional aluminum alloy forms the main structures of the vehicle with some FRP (Fiber Reinforced Plastic) for the skin panels with double curvature. The vehicle is equipped with a completely independent electric system for the automatic landing and it has also an emergency system for ground safety. Ready made devices have been used to reduce the cost and the time needed for manufacture. The results of experiments confirmed that the automatic landing technology was suitable for use in the unmanned vehicle. Significant flight data, including the low speed aerodynamic characteristics have been obtained using this subscale model.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001565003","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL SP-39T","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","subitem_source_identifier_type":"ISSN"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"宇宙開発事業団"},{"subitem_text_value":"宇宙開発事業団"},{"subitem_text_value":"富士重工業"},{"subitem_text_value":"富士重工業"},{"subitem_text_value":"富士重工業"},{"subitem_text_value":"富士重工業"},{"subitem_text_value":"富士重工業"},{"subitem_text_value":"富士重工業"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Space Development Agency of Japan"},{"subitem_text_language":"en","subitem_text_value":"National Space Development Agency of Japan"},{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries Ltd"},{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries Ltd"},{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries Ltd"},{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries Ltd"},{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries Ltd"},{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries Ltd"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"上田, 哲彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"稲葉, 基之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"匂坂, 雅一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"田中, 康平"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"谷川, 栄治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"高井, 政和"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"梅木, 一信"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"木村, 順一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"町田, 茂"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ueda, Tetsuhiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Inaba, Motoyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sagisaka, Masakazu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tanaka, Kohei","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tanikawa, Eiji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takai, Masakazu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Umeki, Kazunobu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kimura, Junichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Machida, Shigeru","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":"2020-02-10"}],"displaytype":"detail","filename":"nalsp0039003.pdf","filesize":[{"value":"4.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0039003.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37206/files/nalsp0039003.pdf"},"version_id":"00baea41-c66b-426d-bbbe-9792d3866118"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"小型自動着陸実験","subitem_subject_scheme":"Other"},{"subitem_subject":"ALFLEX","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE","subitem_subject_scheme":"Other"},{"subitem_subject":"H-2ロケット打上げ型有翼回収機","subitem_subject_scheme":"Other"},{"subitem_subject":"アルミニウム合金","subitem_subject_scheme":"Other"},{"subitem_subject":"FRP","subitem_subject_scheme":"Other"},{"subitem_subject":"繊維強化プラスチック","subitem_subject_scheme":"Other"},{"subitem_subject":"構造システム","subitem_subject_scheme":"Other"},{"subitem_subject":"アクチュエータシステム","subitem_subject_scheme":"Other"},{"subitem_subject":"通信システム","subitem_subject_scheme":"Other"},{"subitem_subject":"計測システム","subitem_subject_scheme":"Other"},{"subitem_subject":"電源システム","subitem_subject_scheme":"Other"},{"subitem_subject":"緊急システム","subitem_subject_scheme":"Other"},{"subitem_subject":"Automatic Landing Flight","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ALFLEX","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"H 2 Orbiting Plane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aluminum alloy","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"FRP","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"fiber reinforced plastic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"structure system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"actuator system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"communication system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"measurement system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"electric power system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"emergency system","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"Development of Automatic Landing Flight Experiment (ALFLEX) vehicle","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Development of Automatic Landing Flight Experiment (ALFLEX) vehicle","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1891","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"37206","relation_version_is_last":true,"title":["Development of Automatic Landing Flight Experiment (ALFLEX) vehicle"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:23:29.724282+00:00"}