{"created":"2023-06-20T14:53:30.834633+00:00","id":21693,"links":{},"metadata":{"_buckets":{"deposit":"fb071cee-afb8-4eaa-93de-905700bbb3b3"},"_deposit":{"created_by":1,"id":"21693","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"21693"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00021693","sets":["1887:1888"]},"author_link":["203675","203673","203672","203674"],"item_7_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Flight Controller Design for Small Quad Tilt Wing UAV"}]},"item_7_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2016-02-05","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"1","bibliographicPageEnd":"82(82)","bibliographicPageStart":"79(79)","bibliographicVolumeNumber":"64","bibliographic_titles":[{"bibliographic_title":"日本航空宇宙学会論文集"},{"bibliographic_title":"Journal of the Japan Society for Aeronautical and Space Sciences","bibliographic_titleLang":"en"}]}]},"item_7_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper is concerned with the design of Stability/Control Augmentation System (S/CAS) for small Quad Tilt Wing (QTW) Unmanned Aerial Vehicle (UAV) which has been developed as a test bed for guidance and control system demonstrations. We design the basic S/CAS for the aircraft using our previously proposed design method. By comparing the eigenvalues of linearized motions of the newly developed and the previously developed QTWUAVs, the effectiveness of our method for S/CAS design is illustrated. We also show the flight test results using our S/CAS.","subitem_description_type":"Other"}]},"item_7_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: 図版あり","subitem_description_type":"Other"}]},"item_7_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains illustrations","subitem_description_type":"Other"}]},"item_7_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: DS1540529012","subitem_description_type":"Other"}]},"item_7_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"Japan Society for Aeronautical and Space Sciences"}]},"item_7_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"日本航空宇宙学会"}]},"item_7_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1344-6460","subitem_source_identifier_type":"ISSN"}]},"item_7_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11307372","subitem_source_identifier_type":"NCID"}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"metadata only access","subitem_access_right_uri":"http://purl.org/coar/access_right/c_14cb"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"佐藤, 昌之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"村岡, 浩治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sato, Masayuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Muraoka, Koji","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Quad Tilt Wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Stability/Control Augmentation System","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Flight Test","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":"journal article","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"小型QTW無人航空機の飛行制御則設計","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"小型QTW無人航空機の飛行制御則設計"}]},"item_type_id":"7","owner":"1","path":["1888"],"pubdate":{"attribute_name":"公開日","attribute_value":"2016-03-28"},"publish_date":"2016-03-28","publish_status":"0","recid":"21693","relation_version_is_last":true,"title":["小型QTW無人航空機の飛行制御則設計"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T03:31:49.818494+00:00"}