DocumentCode
2512686
Title
Supervisory fault tolerant control design for a class of unmanned aerial vehicles
Author
Lu, Lingli ; Jiang, Bin ; Yang, Hao
Author_Institution
Coll. of Autom. Eng., Nanjing Univ. of Aeronaut. & Astronaut., Nanjing, China
fYear
2011
fDate
23-25 May 2011
Firstpage
686
Lastpage
690
Abstract
Traditional fault diagnosis and supervisory fault tolerant control method needs a series of models or filters to isolate the current fault. This may cause the instability of the system due to the isolation time delay. This paper proposes a novel supervisory fault tolerant control scheme for a class of uncertain nonlinear systems with faults ranging over a finite cover. The proposed scheme only relies on a simple switching among a family of pre-computed candidate controllers without any additional models or filters to isolate the faults. The states are ensured to be bounded during the switching delay, which ends when the appropriate stabilizing controller has been selected. An unmanned aerial vehicle example is taken and simulation results are provided to show the efficiency of the proposed method.
Keywords
control system synthesis; delay systems; fault diagnosis; fault tolerance; nonlinear control systems; remotely operated vehicles; space vehicles; stability; uncertain systems; fault diagnosis; fault isolation; filter; isolation time delay; stabilizing controller; supervisory fault tolerant control design; switching delay; system instability; uncertain nonlinear system; unmanned aerial vehicle; Actuators; Fault tolerance; Fault tolerant systems; Nonlinear systems; Switches; Unmanned aerial vehicles; fault diagnosis; supervisory fault tolerant control; switching control; unmanned aerial vehicle;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Decision Conference (CCDC), 2011 Chinese
Conference_Location
Mianyang
Print_ISBN
978-1-4244-8737-0
Type
conf
DOI
10.1109/CCDC.2011.5968270
Filename
5968270
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