• DocumentCode
    2771445
  • Title

    LPV control design for pitch-axis missile autopilots

  • Author

    Wu, Fen ; Packard, Andy ; Balas, Gary

  • Author_Institution
    Centre for Process Syst. Eng., Imperial Coll. of Sci., Technol. & Med., London, UK
  • Volume
    1
  • fYear
    1995
  • fDate
    13-15 Dec 1995
  • Firstpage
    188
  • Abstract
    The missile pitch-axis autopilot is designed using linear parameter-varying (LPV) control theory. The controller guarantees quadratic stability and bounded induced L2-norm performance for the missile plant. Our approach is motivated by gain-scheduling methodology and provides a well founded and systematic procedure for high performance missile autopilot design
  • Keywords
    missile control; stability; stability criteria; LPV control design; bounded induced L2-norm performance; gain-scheduling methodology; linear parameter-varying control; pitch-axis missile autopilots; quadratic stability; Control design; Control system synthesis; Control theory; Design methodology; Educational institutions; Mechanical engineering; Missiles; Open loop systems; Robust control; Robust stability;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 1995., Proceedings of the 34th IEEE Conference on
  • Conference_Location
    New Orleans, LA
  • ISSN
    0191-2216
  • Print_ISBN
    0-7803-2685-7
  • Type

    conf

  • DOI
    10.1109/CDC.1995.478672
  • Filename
    478672
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=2771445