• DocumentCode
    2999563
  • Title

    Research on servo tracking performance of flight simulator

  • Author

    Tang, Zhiyong ; Ding, Yong ; Pei, Zhongcai

  • Author_Institution
    Sch. of Autom. Sci. & Electr. Eng., Beijing Univ. Of Aeronaut. & Astronaut., Beijing
  • fYear
    2008
  • fDate
    1-3 Sept. 2008
  • Firstpage
    1834
  • Lastpage
    1838
  • Abstract
    Because the flight simulator works in different environment for simulating various flight attitudes, the different control algorithm is used for improving the dynamic and static performance. The neural network has good self-learning and self-adaptive, and PID has good robustness, so the adaptive controller based on neural network and PID is used to overcome the coupling inertia and imbalance torque when simulator worked in high speed or large range. And the friction compensation based model reference adaptive control is adopted in low speed status. It has good stability and precision because of using the Stribeck model and Lyapunov stability theory. In order to prove the effectiveness of this controller, experiments have been done.
  • Keywords
    Lyapunov methods; aerospace control; model reference adaptive control systems; neurocontrollers; robust control; servomechanisms; three-term control; Lyapunov stability theory; PID; Stribeck model; flight simulator; friction compensation; model reference adaptive control; neural network; robustness; servo tracking; Adaptive control; Aerospace simulation; Attitude control; Friction; Neural networks; Programmable control; Robust control; Servomechanisms; Three-term control; Torque control; Flight Simulator; compound control; neural network;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Automation and Logistics, 2008. ICAL 2008. IEEE International Conference on
  • Conference_Location
    Qingdao
  • Print_ISBN
    978-1-4244-2502-0
  • Electronic_ISBN
    978-1-4244-2503-7
  • Type

    conf

  • DOI
    10.1109/ICAL.2008.4636456
  • Filename
    4636456