Please use this identifier to cite or link to this item: https://hdl.handle.net/11147/5256
Title: A robust dynamic inversion technique for asymptotic tracking control of an aircraft
Authors: Tanyer, İlker
Tatlıcıoğlu, Enver
Zergeroğlu, Erkan
Keywords: Controllers
Aircraft models
Controller designs
Global asymptotic tracking
Robust dynamic inversions
Issue Date: 2013
Publisher: Institute of Electrical and Electronics Engineers Inc.
Source: Tanyer, İ., Tatlıcıoğlu, E., and Zergeroğlu, E. (2013, June 23-26). A robust dynamic inversion technique for asymptotic tracking control of an aircraft. Paper presented at the 9th Asian Control Conference. doi:10.1109/ASCC.2013.6606263
Abstract: In this paper, a tracking controller is developed for an aircraft model subject to uncertainties in the dynamics and additive state-dependent nonlinear disturbance-like terms. In the design of the controller, dynamic inversion technique is utilized in conjuction with a robust term. Only the output of aircraft dynamics is utilized in the controller design and acceleration measurements are not required. Lyapunov based stability analysis is used to prove global asymptotic tracking. © 2013 IEEE.
Description: 9th Asian Control Conference, ASCC 2013; Istanbul; Turkey; 23 June 2013 through 26 June 2013
URI: http://doi.org/10.1109/ASCC.2013.6606263
http://hdl.handle.net/11147/5256
ISBN: 9781467357692
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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