Title :
Three-dimensional optimal pursuit and evasion with bounded controls
Author :
Shinar, J. ; Gutman, S.
Author_Institution :
Technion--Israel Institute of Technology, Haifa, Israel
fDate :
6/1/1980 12:00:00 AM
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;
Journal_Title :
Automatic Control, IEEE Transactions on
DOI :
10.1109/TAC.1980.1102372