{"created":"2023-06-20T15:10:02.492226+00:00","id":39639,"links":{},"metadata":{"_buckets":{"deposit":"2d5f5d51-cedc-4b33-b891-97ff70383a4f"},"_deposit":{"created_by":1,"id":"39639","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"39639"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00039639","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["443709","443710"],"item_3_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"ウインドシア中の航空機離陸に対するH∞制御"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1995-07","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"7","bibliographicPageStart":"1","bibliographicVolumeNumber":"1273T","bibliographic_titles":[{},{"bibliographic_title":"Technical Report of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"本報告は、ウィンドシア中を離陸する航空機に対する安定化制御則の設計に、最近開発されたH∞制御則設計法を応用した結果について述べる。本報告では、特に状態空間におけるH∞最適制御則構築の定式化を行い、6自由度を持つ飛行シミュレータを用いて異なるウィンドシア時歴および異なる離陸条件に対するシミュレーション試験を行った。その結果、制御対象の航空機はウィンドシア中を安全に離陸できることが分かった。さらに、設計された制御則は、ウィンドシアによる外乱および飛行条件の変化によるモデルパラメータの変動の双方に対してロバストな安定性を持つことが示された。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Results are presented from an application of the most recently developed H infinity control design methodology to a stabilizing controller for an aircraft during take off in a windshear. The emphasis is on the formulating of H infinity optimal control synthesis problem in the state space. Simulation tests are performed in a six degree of freedom flight simulator for different windshear histories and different take off conditions, these results demonstrate that the controlled aircraft could take off in windshear safely, and the designed controller provides stability robustness to both external windshear disturbance as well as the model parameters variation with changes in flight conditions.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000010000","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 TR-1273T","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":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"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 飛行実験部"}]},"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 Research Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"Wang, L."}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Wang, Lixin","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":"2020-01-27"}],"displaytype":"detail","filename":"naltr1273t.pdf","filesize":[{"value":"868.1 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr1273t.pdf","url":"https://jaxa.repo.nii.ac.jp/record/39639/files/naltr1273t.pdf"},"version_id":"0d608ea1-8bfd-4ac1-9b5a-ac8d5f608996"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"ウインドシア","subitem_subject_scheme":"Other"},{"subitem_subject":"H∞制御","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行制御","subitem_subject_scheme":"Other"},{"subitem_subject":"ロバスト制御","subitem_subject_scheme":"Other"},{"subitem_subject":"離陸","subitem_subject_scheme":"Other"},{"subitem_subject":"シミュレーション研究","subitem_subject_scheme":"Other"},{"subitem_subject":"状態空間","subitem_subject_scheme":"Other"},{"subitem_subject":"最適制御","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行安全","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行条件","subitem_subject_scheme":"Other"},{"subitem_subject":"外乱","subitem_subject_scheme":"Other"},{"subitem_subject":"制御装置","subitem_subject_scheme":"Other"},{"subitem_subject":"6自由度","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行シミュレータ","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行経路","subitem_subject_scheme":"Other"},{"subitem_subject":"windshear","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"H infinity control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"robust control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"take off","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"simulation research","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"state space","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"optimal control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight safety","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight condition","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"disturbance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"controller","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"six degree of freedom","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight simulator","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight path","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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"H infinity control for aircraft take off in windshear","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"H infinity control for aircraft take off in windshear","subitem_title_language":"en"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"39639","relation_version_is_last":true,"title":["H infinity control for aircraft take off in windshear"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:20:04.100584+00:00"}