• DocumentCode
    669299
  • Title

    Robust proportional navigation guidance against highly maneuvering targets

  • Author

    Seunghyun Kim ; Kim, H.J.

  • Author_Institution
    Sch. of Mech. & Aerosp. Eng., Seoul Nat. Univ., Seoul, South Korea
  • fYear
    2013
  • fDate
    20-23 Oct. 2013
  • Firstpage
    61
  • Lastpage
    65
  • Abstract
    A robust proportional navigation guidance law is proposed by using Lyapunov approach. Proportional navigation guidance(PNG) law is popularly adopted for missile guidance because it is powerful and simple to implement. In fact, it has been shown that PNG is optimal solution for a stationary target. But PNG performance may sharply degrade in the presence of highly maneuvering target. To find estimation of the miss distance, an optimal approach is used. Then switching control is derived by using this estimation of miss distance. The proposed robust guidance has the form of combination of the conventional PNG and the switching part. Several nonlinear engagement simulations show that the proposed guidance law is robust to the highly maneuvering target.
  • Keywords
    Lyapunov methods; missile guidance; proportional control; robust control; Lyapunov approach; PNG law; maneuvering target; miss distance estimation; missile guidance; nonlinear engagement simulations; robust proportional navigation guidance law; Acceleration; IP networks; Three-dimensional displays; Trajectory; Guidance Law; Miss distance; Robustness;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control, Automation and Systems (ICCAS), 2013 13th International Conference on
  • Conference_Location
    Gwangju
  • ISSN
    2093-7121
  • Print_ISBN
    978-89-93215-05-2
  • Type

    conf

  • DOI
    10.1109/ICCAS.2013.6703864
  • Filename
    6703864