{"id":18739,"date":"2024-12-12T13:33:48","date_gmt":"2024-12-12T13:33:48","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=18739"},"modified":"2024-12-12T13:33:48","modified_gmt":"2024-12-12T13:33:48","slug":"low-cost-wind-tunnel-studies-of-gust-alleviation-control-techniques","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/12\/12\/low-cost-wind-tunnel-studies-of-gust-alleviation-control-techniques\/","title":{"rendered":"LOW-COST WIND TUNNEL STUDIES OF GUST ALLEVIATION CONTROL TECHNIQUES"},"content":{"rendered":"\n<p><strong>B. Barzgaran, J. Quenzer, A. Zongolowicz, K. Hinson, M. Mesbahi, K. Morgansen, E. Livne<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: N\/A<\/strong><\/p>\n\n\n\n<p><strong>Conference number: IFASD-2019-008<\/strong><\/p>\n\n\n\n<p>A low-cost gust load alleviation wind tunnel testing capability has been developed for the University of Washington\u2019s 3ft by 3ft low-speed wind tunnel. The two main components of the resulting system are a \ufb02exible half span wind tunnel model and a gust generation system. The wind tunnel model is an actively-controlled \ufb02exible wing \/ fuselage \/ tail con\ufb01guration. In addition to presenting the system, the paper presents initial gust load alleviation results using Model Predictive Control. The system is versatile by design and allows testing of a wide range of con\ufb01gurations and an extensive selection of control laws at low costs.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2024\/12\/IFASD-2019-008.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>B. Barzgaran, J. Quenzer, A. Zongolowicz, K. Hinson, M. Mesbahi, K. Morgansen, E. Livne<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2019-008<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[2443,2433],"tags":[1972,2799,2021,2800],"class_list":["post-18739","post","type-post","status-publish","format-standard","hentry","category-experimental-active-control","category-1-ifasd-2019","tag-aeroelasticity","tag-optimal-control","tag-structural-dynamics","tag-wind-tunnel-experiments","category-2443","category-2433","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18739","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=18739"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18739\/revisions"}],"predecessor-version":[{"id":18741,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18739\/revisions\/18741"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=18739"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=18739"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=18739"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}