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
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;
Conference_Titel :
American Control Conference, 2002. Proceedings of the 2002
Print_ISBN :
0-7803-7298-0
DOI :
10.1109/ACC.2002.1024546
