Please use this identifier to cite or link to this item: https://hdl.handle.net/11147/5387
Title: A robust adaptive tracking controller for an aircraft with uncertain dynamical terms
Authors: Tanyer, İlker
Tatlıcıoğlu, Enver
Zergeroğlu, Erkan
Keywords: Robust control
Uncertain dynamic systems
Aircrafts
Asymptotic stability
Controllers
Issue Date: 2014
Publisher: Elsevier Ltd.
Source: Tanyer, İ., Tatlıcıoğlu, E., and Zergeroğlu, E. (2014). A robust adaptive tracking controller for an aircraft with uncertain dynamical terms. IFAC Proceedings Volumes, 19, 3202-3207. doi:10.3182/20140824-6-ZA-1003.01515
Abstract: This work presents, the design and the corresponding analysis of a nonlinear controller for an aircraft system subject to uncertainties in the dynamics and additive state-dependent nonlinear disturbance-like terms. Specifically; dynamic inversion technique in conjunction with a robust integral of the signum of the error feedback and an adaptive term is utilized in the overall controller design. Lyapunov based stability analysis techniques are then utilized to prove global asymptotic convergence of the tracking error. © IFAC.
Description: 19th IFAC World Congress on International Federation of Automatic Control, IFAC 2014; Cape Town; South Africa; 24 August 2014 through 29 August 2014
URI: http://doi.org/10.3182/20140824-6-ZA-1003.01515
http://hdl.handle.net/11147/5387
ISSN: 1474-6670
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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