• DocumentCode
    2875667
  • Title

    H∞ controller design of a missile guidance and control system

  • Author

    Wang, Jianwei ; Xie, Xueshu ; Zhong, Yisheng ; Wang, Borong

  • Author_Institution
    Dept. of Autom., Tsinghua Univ., Beijing, China
  • Volume
    5
  • fYear
    1997
  • fDate
    4-6 Jun 1997
  • Firstpage
    2779
  • Abstract
    Presents a case study of H∞ robust controller design of the guidance and control system of an air-to-air missile. Simulations of a simplified linear time-invariant model and a nonlinear time-varying six degree-of-freedom model indicate that the guidance and control system with an H∞ controller can achieve better performance and robustness than that with a proportional navigation amplifier without changing of any other components in the system
  • Keywords
    H∞ control; control system synthesis; linear systems; missile guidance; nonlinear control systems; robust control; time-varying systems; H∞ robust controller; air-to-air missile; missile guidance and control system; nonlinear time-varying six degree-of-freedom model; simplified linear time-invariant model; Acceleration; Automatic control; Control system synthesis; Control systems; Mathematical model; Missiles; Navigation; Proportional control; Robust control; Virtual manufacturing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1997. Proceedings of the 1997
  • Conference_Location
    Albuquerque, NM
  • ISSN
    0743-1619
  • Print_ISBN
    0-7803-3832-4
  • Type

    conf

  • DOI
    10.1109/ACC.1997.611961
  • Filename
    611961
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=2875667