• DocumentCode
    321326
  • Title

    H∞ guidance law with maneuvering targets

  • Author

    Yang, Ciann-Dong ; Chen, Hsin-Yuan

  • Author_Institution
    Inst. of Aeronaut. & Astronaut., Nat. Cheng Kung Univ., Tainan, Taiwan
  • Volume
    3
  • fYear
    1997
  • fDate
    10-12 Dec 1997
  • Firstpage
    2549
  • Abstract
    In this paper we propose an H∞ robust guidance law for homing missiles with maneuvering targets. The nonlinear H∞ suboptimal control design governed by the Hamilton-Jacobi PDE inequality associated with this guidance problem is solved analytically. Based on the existing nonlinear H∞ techniques, we synthesize an H∞ guidance law which can pursue a class of maneuvering targets with acceptable energy consumption and miss distance
  • Keywords
    missile guidance; H∞ guidance law synthesis; H∞ robust guidance law; Hamilton-Jacobi PDE inequality; energy consumption; homing missiles; maneuvering targets; miss distance; nonlinear H∞ suboptimal control design; Attenuation; Control systems; Control theory; Differential equations; Ear; Jacobian matrices; Missiles; Navigation; Robustness; State feedback;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 1997., Proceedings of the 36th IEEE Conference on
  • Conference_Location
    San Diego, CA
  • ISSN
    0191-2216
  • Print_ISBN
    0-7803-4187-2
  • Type

    conf

  • DOI
    10.1109/CDC.1997.657725
  • Filename
    657725
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=321326