• DocumentCode
    3334646
  • Title

    Understanding missile autopilot design using the H∞ loop shaping design procedure

  • Author

    Urban, Thomas J. ; Iwaskiw, Pete ; Iglesias, Pablo A.

  • Author_Institution
    Appl. Phys. Lab., Johns Hopkins Univ., Laurel, MD, USA
  • Volume
    1
  • fYear
    1999
  • fDate
    1999
  • Firstpage
    236
  • Abstract
    This paper presents different controller topologies for a missile autopilot. The controllers are based on a loop shaping design procedure due to McFarlane and Glover. The nature of the controllers obtained is discussed and a novel procedure for the selection of weights is given
  • Keywords
    H∞ control; closed loop systems; control system synthesis; missile control; H∞ loop shaping design procedure; controller topologies; missile autopilot design; weight selection; Acceleration; Control design; Feedback loop; Missiles; Open loop systems; Robust control; Robustness; Shape control; Topology; Tracking loops;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Applications, 1999. Proceedings of the 1999 IEEE International Conference on
  • Conference_Location
    Kohala Coast, HI
  • Print_ISBN
    0-7803-5446-X
  • Type

    conf

  • DOI
    10.1109/CCA.1999.806205
  • Filename
    806205
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=3334646