DocumentCode
2532081
Title
EKF based surface fault detection and reconfiguration in aircraft control systems
Author
Caliskan, F. ; Hajiyev, Ch.M.
Author_Institution
Fac. Electr. Eng., Istanbul Tech. Univ., Turkey
Volume
2
fYear
2000
fDate
2000
Firstpage
1220
Abstract
In this paper, a surface fault detection algorithm based on the extended Kalman filter (EKF) is presented. The innovation, the difference between the actual plant states, and the plant states identified by the EKF are evaluated for the fault detection and identification, and the control reconfiguration procedure is executed by considering the identified control distribution matrix
Keywords
Kalman filters; aircraft control; fault diagnosis; fault tolerance; identification; robust control; aircraft control; control distribution matrix; extended Kalman filter; identification; reconfiguration control; surface fault detection; Aerospace control; Aircraft; Control systems; Covariance matrix; Electrical fault detection; Equations; Fault detection; Fault diagnosis; Noise measurement; Sensor systems;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 2000. Proceedings of the 2000
Conference_Location
Chicago, IL
ISSN
0743-1619
Print_ISBN
0-7803-5519-9
Type
conf
DOI
10.1109/ACC.2000.876694
Filename
876694
Link To Document