• DocumentCode
    584482
  • Title

    Graphical Representation Technology for Knowledge Acquisition of Fault Diagnosis System

  • Author

    Dong, Lei ; Li, Qingdong ; Shao, Xingyue ; Bai, Chen

  • Author_Institution
    Sci. & Technol. on Aircraft Control Lab., Beihang Univ., Beijing, China
  • fYear
    2012
  • fDate
    11-13 Aug. 2012
  • Firstpage
    1627
  • Lastpage
    1630
  • Abstract
    Fault diagnosis expert system (FDES) which can realize high efficient vehicle launch test is an important part of launch protection system in the future space vehicle. The existing way of knowledge acquisition is the artificial extraction rules by knowledge engineers according to the testing process provided by technical personnel. However, this way usually has some problems such as the complexity of the heavy workload, long working cycle, error-prone and does not readily accessible for inspection etc. To solve these problems, this paper presents a method of knowledge acquisition based on graphical representation. Firstly, analysis the testing process of the launch vehicle deeply and establish the overall framework which contains all the preparatory stage subsystem. Then, draw out of the launch vehicle testing process by graphical method through setting reasonable graphical components. This test flow chart is convenient and intuitive to understand, and easier to maintain. Finally, through the design of rule extraction algorithm, the test flow chart is automatically converted to the knowledge which is required by the knowledge base of FDES. This knowledge acquisition method based on graphical techniques can effectively simplify the difficulty, easy to maintain and understand. After testing, this method works well application effect.
  • Keywords
    aerospace expert systems; aerospace safety; aerospace testing; data mining; diagnostic expert systems; fault diagnosis; flowcharting; personnel; space vehicles; FDES; artificial extraction rules; fault diagnosis expert system; graphical components; graphical representation; knowledge acquisition; launch protection system; launch vehicle testing process; rule extraction algorithm design; space vehicle; technical personnel; test flow chart; Expert systems; Fault diagnosis; Knowledge acquisition; Space vehicles; Testing; expert system; fault diagnosis; graphical representation; knowledge acquisition; launch vehicle;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Computer Science & Service System (CSSS), 2012 International Conference on
  • Conference_Location
    Nanjing
  • Print_ISBN
    978-1-4673-0721-5
  • Type

    conf

  • DOI
    10.1109/CSSS.2012.407
  • Filename
    6394646