{"created":"2023-06-20T15:07:50.980499+00:00","id":37212,"links":{},"metadata":{"_buckets":{"deposit":"ef00b3e6-1c44-4e09-a6aa-c83b23f67318"},"_deposit":{"created_by":1,"id":"37212","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37212"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037212","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["479634","479635","479636","479633","479637","479632"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"ジンバル支援システムを用いた拘束飛行試験"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1998-08","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"100","bibliographicPageStart":"95","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":"ALFLEXプロジェクトでは、第1回の自動着陸試験の前に、ジンバル支援システムを使用する拘束飛行試験を数回行なった。これらのテストの目的は、試験機の制御システムの機能と挙動を確認し、その航空力学特性を確認することであった。本報告では、航行制御システムの安定性および性能を研究した。定常飛行試験あるいは疑似静止飛行試験では、小型機姿勢はトリム条件のまわりでよく安定した。迎え角、横滑り角および回転角についてのステップ・コマンド応答は、コンピュータ・シミュレーション結果と一致した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In the ALFLEX project, several constrained flight tests using gimbal support system were conducted before the first automatic landing trial. The purposes of these tests were to confirm the function and performance of the vehicle's control system and to confirm its aerodynamic characteristics. In this report, the stability and performance of the flight control system are studied. In steady or quasi static flight tests, the vehicle attitude was well stabilized around the trimmed condition. The step command responses for angle of attack, side slip angle, and roll angle were consistent with simulation results.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001565009","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":"航空宇宙技術研究所"},{"subitem_text_value":"宇宙開発事業団"}]},"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 Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Space Development Agency of Japan"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"塚本, 太郎"}],"nameIdentifiers":[{"nameIdentifier":"479632","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"柳原, 正明"}],"nameIdentifiers":[{"nameIdentifier":"479633","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"匂坂, 雅一"}],"nameIdentifiers":[{"nameIdentifier":"479634","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Tsukamoto, Taro","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"479635","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Yanagihara, Masaaki","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"479636","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Sagisaka, Masakazu","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"479637","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":"2020-02-10"}],"displaytype":"detail","filename":"nalsp0039009.pdf","filesize":[{"value":"1.9 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0039009.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37212/files/nalsp0039009.pdf"},"version_id":"8b5c81bf-db95-4b52-8eff-1a46bec21f9d"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"ジンバル支援システム","subitem_subject_scheme":"Other"},{"subitem_subject":"拘束飛行","subitem_subject_scheme":"Other"},{"subitem_subject":"ALFLEX","subitem_subject_scheme":"Other"},{"subitem_subject":"小型自動着陸実験","subitem_subject_scheme":"Other"},{"subitem_subject":"航空力学特性","subitem_subject_scheme":"Other"},{"subitem_subject":"航行制御システム","subitem_subject_scheme":"Other"},{"subitem_subject":"疑似静止飛行試験","subitem_subject_scheme":"Other"},{"subitem_subject":"安定性試験","subitem_subject_scheme":"Other"},{"subitem_subject":"迎え角","subitem_subject_scheme":"Other"},{"subitem_subject":"横滑り角","subitem_subject_scheme":"Other"},{"subitem_subject":"回転角","subitem_subject_scheme":"Other"},{"subitem_subject":"コンピュータ・シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"gimbal support system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"constrained flight","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ALFLEX","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Automatic Landing Flight Experiment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight control system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"quasi static flight test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stability test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"angle of attack","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"side slip angle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"roll angle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computer simulation","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":"Constrained flight test with gimbal support system","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Constrained flight test with gimbal support system","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":"37212","relation_version_is_last":true,"title":["Constrained flight test with gimbal support system"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:23:22.576461+00:00"}