DocumentCode
3221667
Title
Design of fault diagnosis expert system for civil aircraft based on FTA-BDD analysis
Author
Ruicheng Guo ; Pu Yang ; Xu Pan
Author_Institution
Coll. of Autom. Eng., Nanjing Univ. of Aeronaut. & Astronaut., Nanjing, China
fYear
2015
fDate
23-25 May 2015
Firstpage
3879
Lastpage
3884
Abstract
According to the different types of faults of the complicated system of civil aircraft, this paper designs a kind of fault diagnosis expert system based on the fault tree analysis. The designing method of each module of knowledge base is given in detail, and the process of calculation is simplified through direct binary decision diagrams (DBDD) method which analyzes component probability importance. The problem of confliction of rules is also solved effectively by introducing a priority coefficient combined with component probability importance and fault diagnosis time. Landing gear retraction system is an example in order to analyze and explain the feasibility of the design of fault diagnosis expert system for civil aircrafts.
Keywords
aerospace engineering; aircraft; binary decision diagrams; expert systems; fault diagnosis; gears; mechanical engineering computing; statistical analysis; FTA-BDD analysis; binary decision diagrams; calculation process; civil aircraft; component probability importance; component probability importance analysis; fault diagnosis expert system design; fault diagnosis time; fault tree analysis; knowledge base module; landing gear retraction system; priority coefficient; rules confliction problem; Aircraft; Data structures; Expert systems; Fault diagnosis; Fault trees; Gears; Probability; Component probability importance; Direct-BDD; FTA; Fault diagnosis expert system; Time cost of fault diagnosis;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Decision Conference (CCDC), 2015 27th Chinese
Conference_Location
Qingdao
Print_ISBN
978-1-4799-7016-2
Type
conf
DOI
10.1109/CCDC.2015.7162601
Filename
7162601
Link To Document