DocumentCode
3248600
Title
Advanced fault diagnosis techniques in aerospace systems
Author
Frank, P.M.
Author_Institution
Duisburg Univ., West Germany
fYear
1989
fDate
8-12 May 1989
Abstract
Discusses the problem of instrument (sensor) fault detection (IFD) in aerospace systems using analytical redundancy. The general framework of model-based fault detection, identification, and accommodation is outlined, and the state of the art in the field is discussed. Emphasis is placed on observer-based residual generation with increased robustness to modeling errors and noise. A time-domain and frequency domain solution to the key problem of designing optimally robust observer schemes on the basis of the unknown input observer theory is described, and the potential of this technique is demonstrated using the example of a flight-control system
Keywords
aerospace control; aerospace instrumentation; aerospace testing; error detection; redundancy; state estimation; IFD; aerospace systems; analytical redundancy; fault detection; fault diagnosis techniques; flight-control system; frequency domain; instrument fault detection; observer schemes; observer-based; residual generation; state estimation; time-domain; Aerospace control; Aircraft; Automatic control; Fault detection; Fault diagnosis; Instruments; Monitoring; Noise robustness; Redundancy; Sensor systems;
fLanguage
English
Publisher
ieee
Conference_Titel
CompEuro '89., 'VLSI and Computer Peripherals. VLSI and Microelectronic Applications in Intelligent Peripherals and their Interconnection Networks', Proceedings.
Conference_Location
Hamburg
Print_ISBN
0-8186-1940-6
Type
conf
DOI
10.1109/CMPEUR.1989.93422
Filename
93422
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