• DocumentCode
    487107
  • Title

    Failure Model Determination in a Knowledge-Based Control System

  • Author

    Huang, Chien Y. ; Stengel, Robert F.

  • Author_Institution
    Princeton University, Department of Mechanical and Aerospace Engineering, Princeton, NJ 08544; Former Graduate student, Grumman Aerospace Corporation
  • fYear
    1987
  • fDate
    10-12 June 1987
  • Firstpage
    1643
  • Lastpage
    1648
  • Abstract
    A technique for determining the most probable failure state of a restructurable control system is presented. The approach is to build a knowledge base that contains and makes use of inference mechanisms to deduce the most likely failures given the symptoms. The analysis is first carried out in a local sense, where only probabilistic information and causality are used to generate failure models, then in a global sense, where the models are grouped and heuristics are used to prune the number of candidate models. Procedures are illustrated using failure patterns of a generic database as well as a fault scenario for a hypothetical helicopter flight control system. It is concluded that the methods are potentially capable of handling generic failures and thus are useful in truly restructable control systems.
  • Keywords
    Aerospace control; Aerospace engineering; Circuit faults; Control system synthesis; Control systems; Databases; Failure analysis; Helicopters; Inference mechanisms; Information analysis;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1987
  • Conference_Location
    Minneapolis, MN, USA
  • Type

    conf

  • Filename
    4789577