DocumentCode
2080340
Title
Structural analysis approach to fault diagnosis with application to fixed-wing aircraft motion
Author
Izadi-Zamanabadi, Roozbeh
Author_Institution
Control Eng. Dept., Aalborg Univ., Denmark
Volume
5
fYear
2002
fDate
2002
Firstpage
3949
Abstract
The paper presents a structural analysis based method for fault diagnosis purposes. The method uses the structural model of the system and utilizes the matching idea to extract system´s inherent redundant information. The structural model is represented by a bipartite directed graph. FDI possibilities are examined by further analysis of the obtained information. The method is illustrated by applying on the LTI model of motion of a fixed-wing aircraft.
Keywords
aircraft control; fault diagnosis; structural engineering; FDI possibilities; LTI model; bipartite directed graph; fault diagnosis; fixed-wing aircraft; fixed-wing aircraft motion; structural analysis approach; structural analysis based method; Aerospace control; Aircraft propulsion; Control engineering; Fault detection; Fault diagnosis; Information analysis; Intelligent control; Intelligent systems; Motion analysis; Sensor systems;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 2002. Proceedings of the 2002
ISSN
0743-1619
Print_ISBN
0-7803-7298-0
Type
conf
DOI
10.1109/ACC.2002.1024546
Filename
1024546
Link To Document