{"id":1099,"date":"2020-04-22T16:24:30","date_gmt":"2020-04-22T16:24:30","guid":{"rendered":"http:\/\/sites.rutgers.edu\/nb-senior-exhibits\/?page_id=1099"},"modified":"2020-04-24T19:56:37","modified_gmt":"2020-04-24T19:56:37","slug":"persikov-nikita-adaptive-fault-tolerant-control-system-design-for-a-fixed-wing-uav","status":"publish","type":"page","link":"https:\/\/sites.rutgers.edu\/nb-senior-exhibits\/partners\/aresty-research-virtual-symposium-2020\/persikov-nikita-adaptive-fault-tolerant-control-system-design-for-a-fixed-wing-uav\/","title":{"rendered":"Persikov, Nikita: Adaptive Fault-Tolerant Control System Design for a Fixed-Wing UAV"},"content":{"rendered":"<p><a href=\"http:\/\/sites.rutgers.edu\/nb-senior-exhibits\/wp-content\/uploads\/sites\/442\/2020\/04\/Nikita_Persikov-poster.pdf\" target=\"_blank\" rel=\"noopener noreferrer\"><img loading=\"lazy\" decoding=\"async\" class=\"size-medium wp-image-691 alignleft\" src=\"http:\/\/sites.rutgers.edu\/nb-senior-exhibits\/wp-content\/uploads\/sites\/442\/2020\/04\/Nikita_Persikov-poster_thumbnail-300x225.png\" alt=\"Nikita Persikov thumbnail\" width=\"300\" height=\"225\" srcset=\"https:\/\/sites.rutgers.edu\/nb-senior-exhibits\/wp-content\/uploads\/sites\/442\/2020\/04\/Nikita_Persikov-poster_thumbnail-300x225.png 300w, https:\/\/sites.rutgers.edu\/nb-senior-exhibits\/wp-content\/uploads\/sites\/442\/2020\/04\/Nikita_Persikov-poster_thumbnail-1024x768.png 1024w, https:\/\/sites.rutgers.edu\/nb-senior-exhibits\/wp-content\/uploads\/sites\/442\/2020\/04\/Nikita_Persikov-poster_thumbnail-768x576.png 768w, https:\/\/sites.rutgers.edu\/nb-senior-exhibits\/wp-content\/uploads\/sites\/442\/2020\/04\/Nikita_Persikov-poster_thumbnail.png 1067w\" sizes=\"(max-width: 300px) 100vw, 300px\" \/><\/a><\/p>\n<p><strong><a class=\"btn btn-primary\" href=\"https:\/\/rutgers.box.com\/s\/3cstyu2z2v5mhzh1bz25tjv91n3sduyx\" target=\"_blank\" rel=\"noopener noreferrer\">View video presentation<\/a><\/strong><\/p>\n<p><strong>Title:<\/strong> Adaptive Fault-Tolerant Control System Design for a Fixed-Wing UAV<\/p>\n<p><strong>Name:<\/strong> Nikita Persikov<\/p>\n<p><strong>Major:<\/strong> Aerospace Engineering<\/p>\n<p><strong>School affiliation:<\/strong> School of Engineering<\/p>\n<p><strong>Programs:<\/strong> JJ Slade Research Program<\/p>\n<p><strong>Other contributors:<\/strong> Laurent Burlion<\/p>\n<p><strong>Abstract:<\/strong> The design of an adaptive control system was obtained by modifying an existing version of a quadcopter control system that allowed for stable \ufb02ight in ideal conditions. The existing roll, pitch and yaw rates were corrected with proportional-integral (PI) controllers. The constant P and I gains were modi\ufb01ed to be time-varying functions, which were derived using the system\u2019s Lyapunov function candidate. After testing on a Simulink model, this system will be uploaded to a Pixhawk-controlled quadcopter to be tested in a hardware-in-the-loop experiment.<\/p>\n","protected":false},"excerpt":{"rendered":"<p>View video presentation Title: Adaptive Fault-Tolerant Control System Design for a Fixed-Wing UAV Name: Nikita Persikov Major: Aerospace Engineering School affiliation: School of Engineering Programs: JJ Slade Research Program Other &hellip; <a href=\"https:\/\/sites.rutgers.edu\/nb-senior-exhibits\/partners\/aresty-research-virtual-symposium-2020\/persikov-nikita-adaptive-fault-tolerant-control-system-design-for-a-fixed-wing-uav\/\" class=\"\">Read More<\/a><\/p>\n","protected":false},"author":970,"featured_media":0,"parent":441,"menu_order":0,"comment_status":"closed","ping_status":"closed","template":"template-custom.php","meta":{"_acf_changed":false,"footnotes":""},"class_list":["post-1099","page","type-page","status-publish","hentry"],"acf":[],"yoast_head":"<!-- This site is optimized with the Yoast SEO plugin v23.5 - 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