DocumentCode
1870099
Title
A fault detection and accommodation framework for dynamic systems with control effector failures
Author
Yang, Hao ; Jiang, Bin ; Wang, Jian Liang
Author_Institution
Coll. of Autom. Eng., Nanjing Univ. of Aeronaut. & Astronaut.
fYear
2006
fDate
19-21 Jan. 2006
Lastpage
1165
Abstract
This paper proposes a novel idea that classifies faults into two different kinds: serious fault and small fault, and treats them with different strategies respectively. A kind of artificial neural network (ANN) is proposed for detecting serious faults, and variable structure (VS) model following control is constructed for accommodating small faults. Moreover, the uncertainty case is investigated and the VS controller is modified. Simulation results of a remotely piloted aircraft with control effector failures illustrate the performance of the developed algorithm
Keywords
aircraft control; failure analysis; fault diagnosis; neural nets; variable structure systems; ANN; VS controller; VS model; accommodation framework; artificial neural network; control effector failures; dynamic systems; fault detection; remotely piloted aircraft; serious fault; small fault; variable structure model; Aerospace control; Aerospace simulation; Aircraft manufacture; Aircraft propulsion; Artificial neural networks; Control system synthesis; Control systems; Differential equations; Fault detection; Uncertainty;
fLanguage
English
Publisher
ieee
Conference_Titel
Systems and Control in Aerospace and Astronautics, 2006. ISSCAA 2006. 1st International Symposium on
Conference_Location
Harbin
Print_ISBN
0-7803-9395-3
Type
conf
DOI
10.1109/ISSCAA.2006.1627572
Filename
1627572
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