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Author Xing-Gang Yan ♦ Edwards, C.
Source IEEE Xplore Digital Library
Content type Text
Publisher Institute of Electrical and Electronics Engineers, Inc. (IEEE)
File Format PDF
Copyright Year ©2005
Language English
Subject Domain (in DDC) Technology ♦ Engineering & allied operations ♦ Other branches of engineering
Subject Keyword Robustness ♦ Actuators ♦ Fault detection ♦ Nonlinear systems ♦ Uncertainty ♦ Nonlinear equations ♦ Aircraft ♦ Control theory ♦ Sliding mode control ♦ Control systems
Abstract In this paper, an actuator fault detection and isolation scheme for a class of nonlinear systems with uncertainty is considered. The uncertainty is allowed to have a nonlinear bound which is a general function of the state variables. A sliding mode observer is established first based on a constrained Lyapunov equation. Then, the equivalent output error injection signal is employed to reconstruct the fault signal using the characteristics of the sliding mode observer and the structure of the uncertainty. Finally, a simulation study of the HIRM aircraft system is presented to show the effectiveness of the scheme.
Description Author affiliation: Control and Instrumentation Research Group, Department of Engineering, University of Leicester, University Road, Leicester, LE1 7RH, UK xy3@le.ac.uk (Xing-Gang Yan)
ISBN 0780395670
Educational Role Student ♦ Teacher
Age Range above 22 year
Educational Use Research ♦ Reading
Education Level UG and PG
Learning Resource Type Article
Publisher Date 2005-12-15
Publisher Place Spain
Rights Holder IEEE/EUCA
Size (in Bytes) 195.62 kB
Page Count 6
Starting Page 987
Ending Page 992


Source: IEEE Xplore Digital Library