• Title of article

    Linear Quadratic Differential Game Strategies with Two-pursuit Versus Single-evader

  • Author/Authors

    LIU، نويسنده , , Yanfang and QI، نويسنده , , Naiming and TANG، نويسنده , , Zhiwei، نويسنده ,

  • Issue Information
    روزنامه با شماره پیاپی سال 2012
  • Pages
    10
  • From page
    896
  • To page
    905
  • Abstract
    In order to intercept the future targets that are characterized by high maneuverability, multiple interceptors may be launched and aimed at single target. The scenario of two missiles P and Q intercepting a single target is modeled as a two-pursuit single-evader non-zero-sum linear quadratic differential game. The intercept space is decomposed into three subspaces which are mutually disjoint and their union covers the entire intercept space. The effect of adding the second interceptor arises in the intercept space of both P and Q (PQ-intercept space). A guidance law is derived from the Nash equilibrium strategy set (NESS) of the game. Simulation studies are focused on the PQ-intercept space. It is indicated that 1) increasing the targetʹs maneuverability will enlarge PQ-intercept space; 2) the handover conditions will be released if the initial zero-effort-miss (ZEM) of both interceptors has opposite sign; 3) overvaluation of the targetʹs maneuverability by choosing a small weight coefficient will generate robust performance with respect to the target maneuvering command switch time and decrease the fuel requirement; and 4) cooperation between interceptors increases the interception probability.
  • Keywords
    Missile , Linear quadratic differential games , two-pursuit single-evader , Guidance , Interception
  • Journal title
    Chinese Journal of Aeronautics
  • Serial Year
    2012
  • Journal title
    Chinese Journal of Aeronautics
  • Record number

    2265200