{"id":17823,"date":"2024-08-14T11:58:28","date_gmt":"2024-08-14T11:58:28","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=17823"},"modified":"2024-08-16T09:18:27","modified_gmt":"2024-08-16T09:18:27","slug":"wind-tunnel-evaluation-of-a-static-output-feedbackcontroller-for-gust-load-alleviation-on-a-regionalaircraft","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/14\/wind-tunnel-evaluation-of-a-static-output-feedbackcontroller-for-gust-load-alleviation-on-a-regionalaircraft\/","title":{"rendered":"WIND TUNNEL EVALUATION OF A STATIC OUTPUT FEEDBACK CONTROLLER FOR GUST LOAD ALLEVIATION ON A REGIONAL AIRCRAFT"},"content":{"rendered":"\n<p><strong>Federico Fonte, Sergio Ricci, Paolo Mantegazza<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: N\/A<\/strong><\/p>\n\n\n\n<p><strong>Conference number: IFASD-2017-068<\/strong><\/p>\n\n\n\n<p>The paper describes the design of a Static Output Feedback (SOF) controller for gust load alleviation and its evaluation on a wind tunnel model of a regional aircraft. The design of the controller is based on the numerical minimization of the 2 norm of the closed loop system. The optimization is performed using a state-space description of the \ufb02exible aircraft which includes also the dynamics of the actuation system and of the sensors. The controller has been evaluated experimentally on a half-span wind tunnel model, in the experimental campaign the robustness of the controller has been evaluated by varying the \ufb02ight condition.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2024\/08\/IFASD-2017-068.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Federico Fonte, Sergio Ricci, Paolo Mantegazza<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-068<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[993,1958,1953],"tags":[2086,2087,684],"class_list":["post-17823","post","type-post","status-publish","format-standard","hentry","category-events","category-dynamic-loads","category-ifasd-2017","tag-gust-load-alleviation","tag-static-output-feedback","tag-wind-tunnel-test","category-993","category-1958","category-1953","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/17823","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/users\/2"}],"replies":[{"embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/comments?post=17823"}],"version-history":[{"count":2,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/17823\/revisions"}],"predecessor-version":[{"id":17922,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/17823\/revisions\/17922"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=17823"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=17823"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=17823"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}