• DocumentCode
    525347
  • Title

    Cross-coupled approach synchronization controller design method based on quantitative feedback theory for dual hydraulic motors driven flight simulators

  • Author

    Guo, Zhifu ; Cao, Jian ; Zhao, Keding

  • Author_Institution
    Sch. of Mechatron. Eng., Harbin Inst. of Technol., Harbin, China
  • Volume
    3
  • fYear
    2010
  • fDate
    25-27 June 2010
  • Abstract
    A novel cross-coupled approach synchronization controller design method is presented for improving whole workspace synchronization of flight simulators. The method synthesizes cross-coupled approach forward channel controllers with QFT (quantitative feedback theory) SISO algorithm. Cross-coupled controllers between two channels are designed using QFT MIMO stability conditions. Synchronization errors are evaluated by steady state synchronization conditions. Additionally, feed forward controllers are adopted to fulfil the strict requirement of magnitude-frequency characteristics and phase-frequency characteristics of flight simulators. Three groups of cross-coupled synchronization controllers are designed according to angle position areas to satisfy performance specification of whole workspace. Simulation results indicate that controllers designed with the proposed method could achieve performance specification requirements over whole workspace.
  • Keywords
    aerospace simulation; feedback; hydraulic motors; synchronisation; MIMO stability condition; SISO algorithm; channel controllers; cross coupled approach; cross coupled synchronization controller; dual hydraulic motor driven flight simulator; feed forward controller; magnitude frequency characteristic; performance specification; phase frequency characteristic; quantitative feedback theory; synchronization controller design method; synchronization error; workspace synchronization; Adaptive control; Aerospace simulation; Computer simulation; Control systems; Design methodology; Error correction; Feedback; Motion control; Optimal control; Programmable control; cross-coupled approach; hydraulic flight simulators; quantitative feedback theory;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Computer Design and Applications (ICCDA), 2010 International Conference on
  • Conference_Location
    Qinhuangdao
  • Print_ISBN
    978-1-4244-7164-5
  • Electronic_ISBN
    978-1-4244-7164-5
  • Type

    conf

  • DOI
    10.1109/ICCDA.2010.5541243
  • Filename
    5541243