• DocumentCode
    832786
  • Title

    Three-dimensional optimal pursuit and evasion with bounded controls

  • Author

    Shinar, J. ; Gutman, S.

  • Author_Institution
    Technion--Israel Institute of Technology, Haifa, Israel
  • Volume
    25
  • Issue
    3
  • fYear
    1980
  • fDate
    6/1/1980 12:00:00 AM
  • Firstpage
    492
  • Lastpage
    496
  • Abstract
    The missile-aircraft pursuit-evasion problem is formulated by a three-dimensional linearized kinematic model with bounded control. The formulation is valid both for the optimal control (against a known adversary strategy) and the zero sum differential game versions. Assuming perfect information, the linearized kinematic model yields for both versions a solution which can be impletemented in real time for airborne application. The avoidance of a known pursuer by an evader who has no state information is solved by a stochastically optimal periodical maneuver. Other examples of imperfect information are briefly discussed.
  • Keywords
    Aircraft control; Differential games; Linear systems, time-varying continuous-time; Missile guidance; Acceleration; Aerodynamics; Aircraft; Geometry; Kinematics; Mathematical model; Missiles; Optimal control; Vehicle dynamics; Vehicles;
  • fLanguage
    English
  • Journal_Title
    Automatic Control, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9286
  • Type

    jour

  • DOI
    10.1109/TAC.1980.1102372
  • Filename
    1102372