• DocumentCode
    530604
  • Title

    Double planes discrete variable structure tracking algorithm

  • Author

    Li, Zhao-Giang ; Zhou, De-Yun ; Wang, Ling-Xiao ; Xu, Jia-Dong

  • Author_Institution
    Dept. of Electron. Inf., Northwestern Polytech. Univ., Xian, China
  • Volume
    4
  • fYear
    2010
  • fDate
    24-26 Aug. 2010
  • Firstpage
    563
  • Lastpage
    566
  • Abstract
    With the development of aviation computer and aviation electronics technologies, the analog tracking algorithm has been unable to meet the need in project. But discrete variable structure tracking algorithm meets the requirement. After go into the sliding mode, the traditional discrete variable structure tracking algorithm will take place of buffeting, and will have phenomenon of the exhale when the front angel is big. In light of the above factors, in order to further improve the precision guided, the no buffeting discrete variable structure double planes tracking algorithm with a compensation of the disturbance is given. The simulation results show that the discrete signal guidance law can meet the tactical UCAV indicator.
  • Keywords
    aerospace control; avionics; discrete systems; variable structure systems; aviation computer; aviation electronics technology; discrete signal guidance law; discrete variable structure; disturbance compensation; double plane tracking algorithm; tactical UCAV indicator; Tracking; discrete signal; double hyperplane; no buffeting; tracking; variable structure control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Computer, Mechatronics, Control and Electronic Engineering (CMCE), 2010 International Conference on
  • Conference_Location
    Changchun
  • Print_ISBN
    978-1-4244-7957-3
  • Type

    conf

  • DOI
    10.1109/CMCE.2010.5610070
  • Filename
    5610070