DocumentCode :
661064
Title :
LPV sliding mode fault tolerant control of an octorotor using fixed control allocation
Author :
Alwi, Halim ; Edwards, Chris
Author_Institution :
Centre for Dynamics & Control, Univ. of Exeter, Exeter, UK
fYear :
2013
fDate :
9-11 Oct. 2013
Firstpage :
772
Lastpage :
777
Abstract :
This paper presents a fault tolerant control scheme for an octorotor using LPV based sliding mode control allocation. The scheme utilizes a combination of sliding mode methods and fixed control allocation in order to deal with rotor faults/failures. An LPV scheme has been used to design the baseline sliding mode controller and a stability analysis has been provided for a wide range of operating conditions. The proposed scheme takes full advantage of the `redundant´ rotors when faults/failures occur, without requiring any FDI (or any information about the faults/failures). Furthermore, the proposed scheme is simple as it does not require the baseline sliding mode controller to be reconfigured. To highlight the efficacy of the proposed scheme, simulation results on a nonlinear octorotor model for various fault/failure scenarios with gust conditions are presented.
Keywords :
aircraft control; control system synthesis; fault diagnosis; fault tolerant control; helicopters; nonlinear control systems; rotors (mechanical); stability; variable structure systems; LPV sliding mode fault tolerant control; fixed control allocation; gust conditions; linear parameter varying analysis; nonlinear octorotor model; octorotor; redundant rotors; rotor failures; rotor faults; sliding mode controller design; stability analysis; Uncertainty;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control and Fault-Tolerant Systems (SysTol), 2013 Conference on
Conference_Location :
Nice
Type :
conf
DOI :
10.1109/SysTol.2013.6693887
Filename :
6693887
Link To Document :
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