• DocumentCode
    3573322
  • Title

    Sliding mode control for turboshaft engine with variable inlet guide vane

  • Author

    Lingfei Xiao ; Renji Gong ; Xinyu Fan ; Yue Zhu

  • Author_Institution
    Jiangsu Province Key Lab. of Aerosp. Power Syst., Nanjing Univ. of Aeronaut. & Astronaut., Nanjing, China
  • fYear
    2014
  • Firstpage
    3972
  • Lastpage
    3976
  • Abstract
    This paper presented a sliding mode controller based on PID reaching law for turboshaft engine with variable inlet guide vane. After analyzing the physical model and mathematical model of compressor elaborately, component-level model of turboshaft engine is obtained. In order to facilitate the turboshaft engine control system design, small deviation linear model of turboshaft engine is achieved based on the component-level model. Taking the unavoidable uncertainties of turboshaft engine into consideration, sliding mode control method is used to construct controller on the basis of PID reaching law. Simulation results validate the effect of the proposed turboshaft engine modeling method and controller design method.
  • Keywords
    blades; control system synthesis; jet engines; linear systems; three-term control; variable structure systems; PID reaching law; component-level model; sliding mode control; small deviation linear model; turboshaft engine control system design; variable inlet guide vane; Blades; Educational institutions; Engines; Mathematical model; Sliding mode control; Turbines; Turboshaft engine; sliding mode control; small deviation linear model; variable inlet guide vane;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Intelligent Control and Automation (WCICA), 2014 11th World Congress on
  • Type

    conf

  • DOI
    10.1109/WCICA.2014.7053380
  • Filename
    7053380