DocumentCode
2581907
Title
Robust actuator fault reconstruction for LPV systems using sliding mode observers
Author
Alwi, Halim ; Edwards, Christopher
Author_Institution
Dept. of Eng., Univ. of Leicester, Leicester, UK
fYear
2010
fDate
15-17 Dec. 2010
Firstpage
84
Lastpage
89
Abstract
This paper presents a fault reconstruction method for LPV systems which is robust against uncertainty and corrupted measurements. The design is analyzed based on a virtual system resulting from factorizing the input distribution matrix associated with the monitored actuators. The key observer parameter (which is used to define the observer gains) is designed using LMIs to minimize the effect of the uncertainty and measurement corruption on the fault reconstruction. The output error injection signals are used to reconstruct the virtual faults, and the input distribution matrix factorization is used to map back to the actual faults. Simulations using an LPV model of a large transport aircraft are presented.
Keywords
actuators; aircraft control; fault diagnosis; linear matrix inequalities; linear systems; matrix decomposition; observers; robust control; variable structure systems; LMI; LPV system; linear parameter varying model; matrix factorization; robust actuator fault reconstruction; sliding mode observer; transport aircraft model; virtual system; Actuators; Aircraft; Atmospheric modeling; Equations; Observers; Robustness; Uncertainty;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control (CDC), 2010 49th IEEE Conference on
Conference_Location
Atlanta, GA
ISSN
0743-1546
Print_ISBN
978-1-4244-7745-6
Type
conf
DOI
10.1109/CDC.2010.5718014
Filename
5718014
Link To Document