• DocumentCode
    1869279
  • Title

    Research on fuzzy variable structure guidance law of the interceptor in aerosphere

  • Author

    Yin, Yongxin ; Yang, Ming ; Wang, Zicai

  • Author_Institution
    Harbin Inst. of Technol., Heilongjiang
  • fYear
    2006
  • fDate
    19-21 Jan. 2006
  • Lastpage
    1377
  • Abstract
    A fuzzy variable structure guidance law has been presented for intercepting the high-speed maneuverable target in aerosphere. The model of the relative movement between target and interceptor has been constructed. Taking the lateral thrust and aerodynamic force combining control into account, a three-dimensional fuzzy guidance law has been designed for tuning the variable structure guidance law, which can ensure the speediness and anti-jamming capability of the system and which can also reduce the chattering. This guidance law needs no information on the velocity and acceleration of the target, and hence is convenient for practical project. The simulation results show that this guidance law has highly precision for high-speed maneuverable target in aerosphere, and show that fuzzy variable structure guidance law has advantage
  • Keywords
    fuzzy control; jamming; military systems; target tracking; variable structure systems; 3D fuzzy guidance law; aerosphere; antijamming capability; chattering; fuzzy variable structure guidance law; high-speed maneuverable target; interceptor; Acceleration; Aerodynamics; Arithmetic; Control systems; Equations; Force control; Fuzzy control; Fuzzy systems; Intelligent control; Kinetic theory;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Systems and Control in Aerospace and Astronautics, 2006. ISSCAA 2006. 1st International Symposium on
  • Conference_Location
    Harbin
  • Print_ISBN
    0-7803-9395-3
  • Type

    conf

  • DOI
    10.1109/ISSCAA.2006.1627540
  • Filename
    1627540