Please use this identifier to cite or link to this item: https://hdl.handle.net/11147/6011
Title: Robust output tracking control of an unmanned aerial vehicle subject to additive state dependent disturbance
Authors: Tanyer, İlker
Tatlıcıoglu, Enver
Zergeroglu, Erkan
Deniz, Meryem
Bayrak, Alper
Özdemirel, Barbaros
Tanyer, İlker
Tatlıcıoglu, Enver
Deniz, Meryem
Özdemirel, Barbaros
Izmir Institute of Technology. Electronics and Communication Engineering
Keywords: Aircraft control
Controllers
Fighter aircraft
Tracking control
Unmanned aerial vehicles
Issue Date: 19-Sep-2016
Publisher: Institution of Engineering and Technology
Source: Tanyer, İ., Tatlıcıoǧlu, E., Zergeroǧlu, E., Deniz, M., Bayrak, A., and Özdemirel, B. (2016). Robust output tracking control of an unmanned aerial vehicle subject to additive state dependent disturbance. IET Control Theory and Applications, 10(14), 1612-1619. doi:10.1049/iet-cta.2015.1304
Abstract: In this study, an asymptotic tracking controller is developed for an aircraft model subject to additive, state-dependent, non-linear disturbance-like terms. Dynamic inversion technique in conjunction with robust integral of the sign of the error term is utilised in the controller design. Compared to the previous studies, the need of acceleration measurements of the aircraft have been removed. In addition, the proposed controller design utilises only the output of aircraft dynamics. Lyapunov based analysis is applied to prove global asymptotic convergence of the tracking error signal. Numerical simulation results are presented to illustrate the performance of the proposed robust controller.
URI: http://doi.org/10.1049/iet-cta.2015.1304
http://hdl.handle.net/11147/6011
ISSN: 1751-8644
1751-8644
Appears in Collections:Electrical - Electronic Engineering / Elektrik - Elektronik Mühendisliği
Scopus İndeksli Yayınlar Koleksiyonu / Scopus Indexed Publications Collection
WoS İndeksli Yayınlar Koleksiyonu / WoS Indexed Publications Collection

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