Robust fault tolerant tracking controller design for a VTOL aircraft

Download
[thumbnail of VerF VTOL aircraft_JFI-SI.pdf]
Preview
VerF VTOL aircraft_JFI-SI.pdf - Accepted Version (674kB) | Preview
Export

Chadli, Mohammed ORCID: 0000-0002-0140-5187, Aouaouda, Sabrina ORCID: 0000-0003-0778-0970, Karimi, Hamid Reza and Shi, Peng ORCID: 0000-0001-8218-586X (2013) Robust fault tolerant tracking controller design for a VTOL aircraft. Journal of the Franklin Institute, 350 (9). pp. 2627-2645. ISSN 0016-0032

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.

Dimensions Badge

Altmetric Badge

Item type Article
URI https://vuir.vu.edu.au/id/eprint/23698
DOI 10.1016/j.jfranklin.2012.09.010
Official URL http://www.sciencedirect.com/science/article/pii/S...
Subjects Historical > FOR Classification > 0102 Applied Mathematics
Historical > FOR Classification > 0901 Aerospace Engineering
Current > Division/Research > College of Science and Engineering
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
Citations in Scopus 111 - View on Scopus
Download/View statistics View download statistics for this item

Search Google Scholar

Repository staff login

CORE (COnnecting REpositories)