{"id":18057,"date":"2024-08-21T11:07:18","date_gmt":"2024-08-21T11:07:18","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=18057"},"modified":"2024-08-21T11:07:19","modified_gmt":"2024-08-21T11:07:19","slug":"application-of-nonlinear-model-order-reduction-technique-to-a-flexible-aircraft-for-real-time-simulations","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/08\/21\/application-of-nonlinear-model-order-reduction-technique-to-a-flexible-aircraft-for-real-time-simulations\/","title":{"rendered":"APPLICATION OF NONLINEAR MODEL ORDER REDUCTION TECHNIQUE TO A FLEXIBLE AIRCRAFT FOR REAL-TIME SIMULATIONS"},"content":{"rendered":"\n<p><strong>Juliano A. Paulino, Fl\u00e1vio J. Silvestre, Ant\u00f4nio B. Guimar\u00e3es Neto, Tiago P. Monteiro, Roberto Gil A. da Silva, Andrea Da Ronch<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: N\/A<\/strong><\/p>\n\n\n\n<p><strong>Conference number: IFASD-2017-152<\/strong><\/p>\n\n\n\n<p>Real\u2013time simulation is a valuable tool for aircraft development. However, \ufb02exible aircraft models are computationally expensive and can be prohibitive for fast simulations. This paper investigates the applicability of a nonlinear model order reduction technique to a moderate \ufb02exible aircraft for real\u2013time simulation purposes. Details of the implementation and test cases are presented. Results show that the reduced\u2013order model can be simulated in real\u2013time and produces better results than linearized model and rigid\u2013body model with aeroelastic correction and we conclude that the technique is promising for real\u2013time simulations.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2024\/08\/IFASD-2017-152.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Juliano A. Paulino, Fl\u00e1vio J. Silvestre, Ant\u00f4nio B. Guimar\u00e3es Neto, Tiago P. Monteiro, Roberto Gil A. da Silva, Andrea Da Ronch<b\/><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: IFASD-2017-152<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[993,1953,1962],"tags":[2255,2105,2104,2256],"class_list":["post-18057","post","type-post","status-publish","format-standard","hentry","category-events","category-ifasd-2017","category-reduced-order-modeling","tag-aeroelasticity-real-time-simulation","tag-exible-aircraft","tag-ight-dynamics","tag-reduced-order-modeling-2","category-993","category-1953","category-1962","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18057","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=18057"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18057\/revisions"}],"predecessor-version":[{"id":18059,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/18057\/revisions\/18059"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=18057"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=18057"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=18057"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}