DocumentCode
3484796
Title
Integral sliding mode fault tolerant control incorporating on-line control allocation
Author
Hamayun, Mirza Tariq ; Edwards, Christopher ; Alwi, Halim
Author_Institution
Control & Instrum. Res. Group, Univ. of Leicester, Leicester, UK
fYear
2010
fDate
26-28 June 2010
Firstpage
100
Lastpage
105
Abstract
This paper proposes a novel integral sliding mode on-line control allocation scheme for fault tolerant control. The order of the sliding motion in the sliding mode is not reduced as in conventional sliding mode schemes. Also the robustness of the closed loop system can be guaranteed throughout the entire response, starting from the initial time instant, because there is no reaching phase. Actuator effectiveness levels are used to redistribute the control signals to healthy actuators online in the case of faults or failures without reconfiguring the controller. In this way the scheme can cope with total failure of certain actuators. Simulation results using the Admire aircraft model show good performance in fault and even certain total actuator failure scenarios which validates the effectiveness and feasibility of the proposed scheme.
Keywords
actuators; aircraft control; closed loop systems; fault tolerance; robust control; variable structure systems; actuator effectiveness levels; actuator failure; admire aircraft model; closed loop system; control signals; healthy actuators; initial time instant; integral sliding mode fault tolerant control; online control allocation; robustness; sliding motion; Actuators; Aircraft; Automatic control; Control systems; Fault tolerance; Fault tolerant systems; Robustness; Sliding mode control; Stability; Testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Variable Structure Systems (VSS), 2010 11th International Workshop on
Conference_Location
Mexico City
Print_ISBN
978-1-4244-5829-5
Electronic_ISBN
978-1-4244-5830-1
Type
conf
DOI
10.1109/VSS.2010.5544704
Filename
5544704
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