• DocumentCode
    2279461
  • Title

    Robust H-infinity Tracing Control of 3-DOF Helicopter Model

  • Author

    Wang Xiuyan ; Zhao Changli ; Li Zongshuai

  • Author_Institution
    Civil Aviation Univ. of China, Tianjin, China
  • Volume
    3
  • fYear
    2010
  • fDate
    13-14 March 2010
  • Firstpage
    279
  • Lastpage
    282
  • Abstract
    The stability and anti-jamming of 3-DOF helicopter model system are weak because of non-linearity and parameter uncertainty, so H-infinity mixed sensitivity laws are adopted to design trajectory tracking controller. Firstly, the bounded non-linear parameters are transformed into the uncertainty of parameters and added by inherent parameters perturbation it composes the linear uncertainty model. The H-infinity control method based on mixed sensitivity is adopted. By setting the weighting function of sensitivity and complementary sensitivity, the multitask controller of disturbance rejection and robust tracking is translated to a stander H-infinity controller of regulate problem. Simulation results demonstrate that the trajectory of helicopter attitude tracks well and system robust stability is improved.
  • Keywords
    H¿ control; helicopters; position control; stability; 3DOF helicopter model; parameter uncertainty; robust H-infinity tracing control; robust stability; robust tracking; trajectory tracking controller; weighting function; Equations; Fuzzy logic; H infinity control; Helicopters; Optimal control; Robust control; Robust stability; Trajectory; Uncertain systems; Uncertainty; Mixed Sensitivity and Uncertainty; Three-degree of Freedom Helicopter; Trajectory Tracking;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Measuring Technology and Mechatronics Automation (ICMTMA), 2010 International Conference on
  • Conference_Location
    Changsha City
  • Print_ISBN
    978-1-4244-5001-5
  • Electronic_ISBN
    978-1-4244-5739-7
  • Type

    conf

  • DOI
    10.1109/ICMTMA.2010.613
  • Filename
    5458690