DocumentCode :
2247007
Title :
The Missile Flight Control System reliability analysis based on hybrid fault trees
Author :
Yuan Jing ; Long Yong
Author_Institution :
Xi´an Res. Inst. of Hi-tech Hongqing Town, Xi´an, China
Volume :
3
fYear :
2010
fDate :
6-7 March 2010
Firstpage :
158
Lastpage :
160
Abstract :
As Missile Flight Control System (MFCS) is a typical complex and high reliable system, its safety and reliability has been turn into an all-important problem. MFCS is frequently employed high level of redundancy for achieving high level of reliability. Dynamic redundancy employed in MFCS can realize complex fault and error diagnosis, recovery and reconfiguration. It is very difficult to analyze the reliability of MFCS by traditional Fault Tree Analysis (FTA) methods. This paper analyzes the weakness of FTA and induces a method of Hybrid FTA that combine dynamic fault tree. Accordingly, static FTA uses binary decision diagrams and dynamic FTA uses Markov Chains. At last, an example is proposed to prove academic analysis.
Keywords :
Markov processes; binary decision diagrams; fault diagnosis; fault trees; large-scale systems; missile control; FTA; Markov chains; binary decision diagrams; complex system; dynamic fault tree; dynamic redundancy; error diagnosis; fault diagnosis; fault tree analysis; hybrid fault trees; missile flight control system reliability analysis; Aerospace control; Aerospace safety; Control system analysis; Data structures; Fault diagnosis; Fault trees; Missiles; Redundancy; Reliability; US Department of Transportation; Missile flight control system; Reliability; hybrid fault tree;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Informatics in Control, Automation and Robotics (CAR), 2010 2nd International Asia Conference on
Conference_Location :
Wuhan
ISSN :
1948-3414
Print_ISBN :
978-1-4244-5192-0
Electronic_ISBN :
1948-3414
Type :
conf
DOI :
10.1109/CAR.2010.5456653
Filename :
5456653
Link To Document :
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