• DocumentCode
    1831466
  • Title

    UIO-based diagnosis of aircraft engine control systems using scilab

  • Author

    Liu, Yue ; Tan, Daoliang ; He, Ai ; Wang, Xi

  • Author_Institution
    Sch. of Jet Propulsion, Beihang Univ., Beijing, China
  • fYear
    2011
  • fDate
    12-14 Oct. 2011
  • Firstpage
    64
  • Lastpage
    70
  • Abstract
    Fault diagnosis is of significant importance to the robustness of aeroengine control systems. This paper makes use of full-order unknown input observers (UIOs) to facilitate the diagnosis of sensor/actuator faults in engine control systems. The built-in “ui-observer” function in Scilab, however, can not give satisfying performance, in terms of observer realization. Hence we rewrite this UIO program in standard Scilab scripts and decouple the effect of unknown disturbances upon state estimation to improve the sensitivity to engine faults. An evaluation platform is created on the basis of the Xcos tool in a Simulink-like manner. All the above work is accomplished in the Scilab environment. Experimental results on an aircraft turbofan engine demonstrate that the suggested UIO diagnostic method has good anti-disturbance ability and can effectively detect and isolate sensor/actuator faults under various fault conditions.
  • Keywords
    aerospace control; aerospace engines; estimation theory; fault diagnosis; observers; Scilab scripts; Simulink-like manner; UIO based diagnosis; Xcos tool; aircraft engine control systems; aircraft turbofan engine; fault diagnosis; full-order unknown input observers; observer realization; scilab; state estimation; Actuators; Aircraft propulsion; Engines; Mathematical model; Robustness; Vectors; UIO; Xcos; aircraft engine simulation; fault detection; fault diagnosis;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Open-Source Software for Scientific Computation (OSSC), 2011 International Workshop on
  • Conference_Location
    Beijing
  • Print_ISBN
    978-1-61284-492-3
  • Type

    conf

  • DOI
    10.1109/OSSC.2011.6184696
  • Filename
    6184696