• DocumentCode
    300503
  • Title

    Loop shaping design of a robust missile autopilot

  • Author

    White, B A ; Patel, Y. ; Vorley, D.H. ; Horton, M.

  • Author_Institution
    R. Mil. Coll. of Sci., Shrivenham, UK
  • Volume
    1
  • fYear
    1995
  • fDate
    21-23 Jun 1995
  • Firstpage
    520
  • Abstract
    An H∞ controller is designed for a latax autopilot missile, using the method of loop shaping and the central K algorithm of McFarlane and Glover (1989). The resulting autopilot is shown to have good robustness to variations in incidence and roll angle
  • Keywords
    H∞ control; control system synthesis; missile guidance; robust control; H∞ controller; central K algorithm; latax autopilot missile; loop shaping design; robust missile autopilot; robustness; Algorithm design and analysis; Centralized control; Closed loop systems; Instruments; Missiles; Open loop systems; Robust stability; Robustness; Shape control; Steady-state;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, Proceedings of the 1995
  • Conference_Location
    Seattle, WA
  • Print_ISBN
    0-7803-2445-5
  • Type

    conf

  • DOI
    10.1109/ACC.1995.529303
  • Filename
    529303
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=300503