• DocumentCode
    3026450
  • Title

    Recent advances in optimal pursuit and evasion

  • Author

    Shinar, J. ; Gutman, S.

  • Author_Institution
    Technion, Israel Institute of Technology, Haifa, Israel
  • fYear
    1979
  • fDate
    10-12 Jan. 1979
  • Firstpage
    960
  • Lastpage
    965
  • Abstract
    The missile-aircraft pursuit-evasion problem is formulated by a three-dimensional linearized kinematic model. 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 implemented 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
    Acceleration; Aerodynamics; Kinematics; Missiles; Optimal control; Vehicle dynamics;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control including the 17th Symposium on Adaptive Processes, 1978 IEEE Conference on
  • Conference_Location
    San Diego, CA, USA
  • Type

    conf

  • DOI
    10.1109/CDC.1978.268074
  • Filename
    4046261