DocumentCode
2917672
Title
Fault tolerant control of an octorotor using LPV based sliding mode control allocation
Author
Alwi, Halim ; Edwards, Chris
Author_Institution
Dept. of Eng., Univ. of Leicester, Leicester, UK
fYear
2013
fDate
17-19 June 2013
Firstpage
6505
Lastpage
6510
Abstract
This paper presents an LPV based sliding mode fault tolerant controller for an octorotor. The scheme utilizes a combination of sliding mode methods and 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 coverage of operating conditions. The proposed scheme uses control allocation to take full advantage of the `redundant´ rotors to redistribute the control signals to the healthy rotors when faults/failures occur. Simulation results on the nonlinear model for various fault/failure scenarios show no visible difference in comparison to the nominal fault free performance.
Keywords
aircraft control; autonomous aerial vehicles; fault tolerance; helicopters; mobile robots; rotors; stability; telerobotics; variable structure systems; LPV based sliding mode control allocation; UAV; baseline sliding mode controller design; control signal redistribution; fault free performance; multirotor unmanned aerial vehicle; nonlinear model; octorotor; redundant rotors; rotor fault-failure; sliding mode fault tolerant controller; stability analysis; Actuators; Equations; Fault tolerance; Mathematical model; Resource management; Rotors; Uncertainty;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference (ACC), 2013
Conference_Location
Washington, DC
ISSN
0743-1619
Print_ISBN
978-1-4799-0177-7
Type
conf
DOI
10.1109/ACC.2013.6580859
Filename
6580859
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