Please use this identifier to cite or link to this item: https://hdl.handle.net/20.500.11851/2827
Title: Stabilizer Autopilot Design For Fixed Wing UAV Using ODSMC
Authors: Güneş, Uygar
Sel, Artun
Kasnakoğlu, Coşku
Keywords: UAV
ODSMC
Issue Date: 2018
Publisher: IEEE
Source: Güneş, U., Artun, S. E. L., and Kasnakoğlu, C. (2018, October). Stabilizer Autopilot Design For Fixed Wing UAV Using ODSMC. In 2018 22nd International Conference on System Theory, Control and Computing (ICSTCC) (pp. 740-746). IEEE.
Abstract: In this paper we build an ODSMC (Output Feedback Discrete Time Sliding Mode Control) controller for a fixed-winged aircraft. ODSMC control is employed, which is widely utilized in commercial and reconnaissance applications. The small-disturbance theory is used to obtain the mathematical model of the system which has highly nonlinear and non minimum characteristics. The ODSMC, due to its dynamic structure has been proved to be better than conventional linear controllers. Because of its output feedback structure, it also eliminates the need for a state observer. The ODSMC is designed based on the obtained linear model of the given plant. The effectiveness of the aircraft control system is analyzed by means of numerical simulations. The ODSMC control algorithm gives quite satisfactory results regarding the disturbance rejection capability of the closed loop system.
URI: https://hdl.handle.net/20.500.11851/2827
https://ieeexplore.ieee.org/document/8540682
ISBN: 978-1-5386-4444-7
ISSN: 2372-1618
Appears in Collections:Elektrik ve Elektronik Mühendisliği Bölümü / Department of Electrical & Electronics Engineering
Scopus İndeksli Yayınlar Koleksiyonu / Scopus Indexed Publications Collection
WoS İndeksli Yayınlar Koleksiyonu / WoS Indexed Publications Collection

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