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Robust fault tolerant tracking controller design for a VTOL aircraft

Chadli, M and Aouaouda, S and Karimi, Hamid Reza and Shi, Peng (2013) Robust fault tolerant tracking controller design for a VTOL aircraft. Journal of the Franklin Institute, 350 (9). pp. 2627-2645. ISSN 0016-0032

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Abstract

In the last three decades, the need for increased flight safety and aircraft reliability has been and will continue to be an important issue in commercial aviation industry. All pilots undergo widespread training to help them to be able to react to unexpected difficulties that may occur during a flight in uncertain conditions. Furthermore, advanced fault-tolerant control (FTC) systems are designed to help pilots overcome abnormal situations that previously might have resulted in catastrophic events.

Item Type: Article
Uncontrolled Keywords: ResPubID26683, ResPubID25484, fault tolerant control design, FTC, vertical takeoff and landing, tolerance, aircrafts, external disturbances, actuator faults, trajectory tracking, Takagi–Sugeno model, mathematical models, linear matrix inequalities
Subjects: FOR Classification > 0102 Applied Mathematics
FOR Classification > 0901 Aerospace Engineering
Faculty/School/Research Centre/Department > College of Science and Engineering
Depositing User: Ms Phung.T Tran
Date Deposited: 22 Dec 2013 22:42
Last Modified: 10 Mar 2015 03:37
URI: http://vuir.vu.edu.au/id/eprint/23698
DOI: 10.1016/j.jfranklin.2012.09.010
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Citations in Scopus: 6 - View on Scopus

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