DESIGN OF FRACTIONAL ORDER SLIDING MODE CONTROLLER FOR 2 DOF HELICOPTER SYSTEM

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dc.contributor.authorKavuran, Gürkan
dc.contributor.authorYeroğlu, Celaleddin
dc.date.accessioned2024-08-04T19:51:33Z
dc.date.available2024-08-04T19:51:33Z
dc.date.issued2018
dc.departmentİnönü Üniversitesien_US
dc.description.abstractThis paper presents a real time control application for a prototype helicopter system by using Sliding Mode Controlstrategy modified with small differential deviations. Experimental and simulation studies demonstrate theperformanceof the proposed controller for a class of flight systems with unstable dynamics. It is shown that theproposed controller decreases the steady state errors of the vertical and horizontal motion of the system. Smalldifferential deviations strengthen or weaken the effect of the differential to obtain better tracking response in case ofexternal disturbances. Numerical and experimental results match each otherto demonstratethe tracking of desiredrotor angles and suppression the disturbance effects.en_US
dc.identifier.endpage47en_US
dc.identifier.issn1304-0448
dc.identifier.issn2148-1059
dc.identifier.issue2en_US
dc.identifier.startpage35en_US
dc.identifier.trdizinid287643en_US
dc.identifier.urihttps://search.trdizin.gov.tr/yayin/detay/287643
dc.identifier.urihttps://hdl.handle.net/11616/89061
dc.identifier.volume11en_US
dc.indekslendigikaynakTR-Dizinen_US
dc.language.isoenen_US
dc.relation.ispartofHavacılık ve Uzay Teknolojileri Dergisien_US
dc.relation.publicationcategoryMakale - Ulusal Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/openAccessen_US
dc.titleDESIGN OF FRACTIONAL ORDER SLIDING MODE CONTROLLER FOR 2 DOF HELICOPTER SYSTEMen_US
dc.typeArticleen_US

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