DocumentCode
3532716
Title
Fault Prognosis Modeling of Aviation Electronic System Based on Kalman Filtering
Author
Kong Qing-chun ; Xiao Ming-qing ; Zhao Xin
Author_Institution
Eng. Sch., Air Force Eng. Univ., Xi´an
fYear
2009
fDate
28-29 April 2009
Firstpage
1
Lastpage
4
Abstract
According to characteristics of fault in aviation electronic system, first of all, fault prognosis model based on Kalman filtering is established and analyzed in this paper, a certain method of to determine fault point critical status value is given, and then a project for fault prognosis is decided and fault prognosis algorithm is designed. And at last, historical data in system operation and test is fully utilized by fault prognosis model, and by so doing a theoretical foundation is provided for predicting fault and performance.
Keywords
Kalman filters; avionics; built-in self test; Kalman filtering; aviation electronic system; condition-based maintenance; fault prognosis modeling; Aerospace electronics; Algorithm design and analysis; Control system synthesis; Design engineering; Fault detection; Filtering; Kalman filters; Maintenance; Modeling; System testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Testing and Diagnosis, 2009. ICTD 2009. IEEE Circuits and Systems International Conference on
Conference_Location
Chengdu
Print_ISBN
978-1-4244-2587-7
Type
conf
DOI
10.1109/CAS-ICTD.2009.4960822
Filename
4960822
Link To Document