• DocumentCode
    1600835
  • Title

    Robust full-envelope missile autopilot design

  • Author

    Juang, Jyh-Ching ; Lin, Ching-Fang ; Cloutier, James R. ; Evers, Johnny H.

  • Author_Institution
    American GNC Corp., Chatsworth, CA, USA
  • fYear
    1992
  • Firstpage
    231
  • Abstract
    The design of a robust full-envelope autopilot for the HAVE DASH II missile system is delineated. Existing control design methods are examined and integrated to meet the stringent performance requirements of the missile autopilot design
  • Keywords
    control system synthesis; missiles; stability; HAVE DASH II missile system; control design methods; performance requirements; robust full-envelope autopilot; Aerodynamics; Design methodology; Missiles; Observability; Robust control; Robust stability; Robustness; Uncertainty; Velocity control; Virtual manufacturing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Applications, 1992., First IEEE Conference on
  • Conference_Location
    Dayton, OH
  • Print_ISBN
    0-7803-0047-5
  • Type

    conf

  • DOI
    10.1109/CCA.1992.269871
  • Filename
    269871