• DocumentCode
    2780496
  • Title

    A game theoretical interceptor guidance law for ballistic missile defence

  • Author

    Shinar, J. ; Shima, T.

  • Author_Institution
    Fac. of Aerosp. Eng., Technion-Israel Inst. of Technol., Haifa, Israel
  • Volume
    3
  • fYear
    1996
  • fDate
    11-13 Dec 1996
  • Firstpage
    2780
  • Abstract
    Defence scenarios against manoeuvrable tactical ballistic missiles are formulated as imperfect information zero-sum pursuit-evasion games. Both missiles, the “blind” tactical ballistic missile (evader) and the interceptor (pursuer) have first-order dynamics. The interceptor guidance law is based on the perfect information game solution, assuming target manoeuvre knowledge, and has a point capture (robust “hit-to-kill” accuracy) potential. The estimation process of the evader´s manoeuvre is approximated by a delayed perfect information outcome. The paper evaluates the effect of estimation delay on the guidance performance and outlines a methodology to assess the probability of interception avoidance by randomly manoeuvring evaders
  • Keywords
    dynamics; game theory; missile guidance; probability; dynamics; estimation delay; game theory; interceptor guidance law; probability; tactical ballistic missiles; target manoeuvre; zero-sum pursuit-evasion games; Aerodynamics; Aerospace engineering; Aircraft; Delay effects; Delay estimation; Game theory; Information analysis; Missiles; Robustness; Trajectory;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 1996., Proceedings of the 35th IEEE Conference on
  • Conference_Location
    Kobe
  • ISSN
    0191-2216
  • Print_ISBN
    0-7803-3590-2
  • Type

    conf

  • DOI
    10.1109/CDC.1996.573534
  • Filename
    573534