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dc.contributor.authorKanat, Oztuerk Ozdemir
dc.contributor.authorKaratay, Ertugrul
dc.contributor.authorKose, Oguz
dc.contributor.authorOktay, Tugrul
dc.date.accessioned2021-11-09T19:49:15Z
dc.date.available2021-11-09T19:49:15Z
dc.date.issued2019
dc.identifier.issn0954-4100
dc.identifier.issn2041-3025
dc.identifier.urihttps://doi.org/10.1177/0954410019846045
dc.identifier.urihttps://hdl.handle.net/20.500.12440/3984
dc.description.abstractIn this article, combined active flow control system and flight control system design for morphing unmanned aerial vehicles is applied for the first time for autonomous flight performance maximization. For this purpose, longitudinal and lateral dynamics modeling of morphing unmanned aerial vehicle having active flow control manufactured in Erciyes University, Faculty of Aeronautics and Astronautics, Model Aircraft Laboratory is considered in order to obtain simulation environments. Our produced morphing unmanned aerial vehicle is called as ZANKA-II, which has a mass of 6.5 kg, range of 30 km, endurance of 0.5 h, and ceiling altitude of 6000 m. von Karman turbulence modeling is used in order to model atmospheric turbulence during flight in both longitudinal and lateral simulation environments. A stochastic optimization method called as simultaneous perturbation stochastic approximation is also applied for the first time in order to obtain optimum dimensions of morphing parameters (i.e. extension ratios of wingspan and tail span), optimum positions of blowers, and optimum magnitudes of longitudinal and lateral controllers' gains (i.e. P, I, and D gains) while minimizing cost index capturing terms for both longitudinal and lateral autonomous flight performances and there exist lower and upper constraints on all optimization variables in the literature.en_US
dc.language.isoengen_US
dc.publisherSage Publications Ltden_US
dc.relation.ispartofProceedings of The Institution of Mechanical Engineers Part G-Journal of Aerospace Engineeringen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectAutomatic controlen_US
dc.subjectactive flow controlen_US
dc.subjectclosed-loop systemen_US
dc.subjectcontrol systemen_US
dc.subjectmotion controlen_US
dc.subjectproportional-integral-derivative controlen_US
dc.subjectmorphingen_US
dc.titleCombined active flow and flight control systems design for morphing unmanned aerial vehiclesen_US
dc.typearticleen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.description.wospublicationidWOS:000483588200025en_US
dc.description.scopuspublicationid2-s2.0-85065442362en_US
dc.departmentGümüşhane Üniversitesien_US
dc.authoridOKTAY, TUGRUL / 0000-0003-4860-2230
dc.identifier.volume233en_US
dc.identifier.issue14en_US
dc.identifier.startpage5393en_US
dc.identifier.doi10.1177/0954410019846045
dc.identifier.endpage5402en_US
dc.authorwosidOKTAY, TUGRUL / AAE-2053-2020
dc.authorscopusid57208282131
dc.authorscopusid57208650091
dc.authorscopusid57211985357
dc.authorscopusid55334339800


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