• DocumentCode
    3238975
  • Title

    Flight simulator servo system friction compensation based on variable structure control

  • Author

    Liang-yu, Su ; Wu, Wang

  • Author_Institution
    Sch. of Electr. & Inf. Eng., Xuchang Univ., Xuchang, China
  • fYear
    2011
  • fDate
    27-29 May 2011
  • Firstpage
    645
  • Lastpage
    648
  • Abstract
    As friction is the main nonlinear resistance in the flight simulator servo system which can lead to overall flight simulator performance degradation. The mathematical model of flight simulator servo system was created based on a three-axis servo system and the LuGre friction model was analyzed. Exponential approach law was introduced into variable structure control and the robust controller was realized. The simulation result shows the sliding mode controller has superior position tracking and speed tracking performance for low speed servo system with friction compensated effectively.
  • Keywords
    aerospace control; aerospace simulation; compensation; friction; nonlinear control systems; position control; robust control; servomechanisms; variable structure systems; velocity control; LuGre friction model; flight simulator performance degradation; flight simulator servo system friction compensation; mathematical model; nonlinear resistance; position tracking; robust controller; sliding mode controller; speed tracking; three-axis servo system; variable structure control; Friction; Inductance; Servomotors; flight simulator servo system; friction model; simulation; variable structure control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Communication Software and Networks (ICCSN), 2011 IEEE 3rd International Conference on
  • Conference_Location
    Xi´an
  • Print_ISBN
    978-1-61284-485-5
  • Type

    conf

  • DOI
    10.1109/ICCSN.2011.6014652
  • Filename
    6014652