• DocumentCode
    3070118
  • Title

    Robust stability analysis of a lateral flight control system for a missile

  • Author

    White, Brian A. ; Tsourdos, Antonios

  • Author_Institution
    Dept. of Aerosp. Power & Sensors, R. Mil. Coll. of Sci., Shrivenham, UK
  • Volume
    6
  • fYear
    1999
  • fDate
    1999
  • Firstpage
    3748
  • Abstract
    A homing missile lateral autopilot is synthesized by exploiting the fact that under mild differentiability conditions, nonlinear systems can be represented in quasilinear form. The robustness of the lateral missile velocity autopilot to uncertain aerodynamic parameters is then determined using Kharitonov´s theorem
  • Keywords
    control system analysis; control system synthesis; missile control; nonlinear control systems; robust control; velocity control; Kharitonov´s theorem; homing missile lateral autopilot; lateral flight control system; mild differentiability conditions; robust stability analysis; robustness; uncertain aerodynamic parameters; velocity autopilot; Adaptive control; Aerodynamics; Aerospace control; Control system synthesis; Missiles; Nonlinear equations; Robust stability; Robustness; Sensor systems; Velocity control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1999. Proceedings of the 1999
  • Conference_Location
    San Diego, CA
  • ISSN
    0743-1619
  • Print_ISBN
    0-7803-4990-3
  • Type

    conf

  • DOI
    10.1109/ACC.1999.786199
  • Filename
    786199
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=3070118