DocumentCode
696203
Title
Linear matrix inequality based static output feedback sliding mode control for discrete time systems
Author
Govindaswamy, Srinath ; Floquet, Thierry ; Spurgeon, Sarah K.
Author_Institution
Dept. of Electron., Univ. of Kent, Canterbury, UK
fYear
2009
fDate
23-26 Aug. 2009
Firstpage
2722
Lastpage
2727
Abstract
This paper discusses the design of a static output feedback based sliding mode controller for MIMO non-minimum phase discrete time systems. In previous work, it was shown that by identifying a minimal set of current and past outputs to determine an extended output signal, an augmented system can be obtained which permits the design of a sliding manifold based upon output information only, which renders the sliding mode dynamics stable. In this paper, it is shown that if the extended outputs chosen span the state zero directions of an invariant zero of the system, then the invariant zero disappears from the augmented system. Linear matrix inequalities are then used for sliding surface design. Such controllers have great potential within reconfigurable control schemes for application in the presence of multiple sensor failures. The methodology is applied to an aircraft system to show the efficacy of the design philosophy.
Keywords
MIMO systems; aircraft control; control system synthesis; discrete time systems; feedback; linear matrix inequalities; variable structure systems; MIMO nonminimum phase discrete time systems; aircraft system; augmented system; design philosophy; invariant zero; linear matrix inequalities; reconfigurable control schemes; sensor failures; sliding surface design; state zero directions; static output feedback based sliding mode controller design; Aerospace electronics; Discrete-time systems; Europe; Linear matrix inequalities; Output feedback; Sliding mode control;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (ECC), 2009 European
Conference_Location
Budapest
Print_ISBN
978-3-9524173-9-3
Type
conf
Filename
7074818
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