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Three-dimensional optimal pursuit and evasion with bounded controls

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2 Author(s)
Shinar, J. ; Technion--Israel Institute of Technology, Haifa, Israel ; Gutman, S.

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.

Published in:

Automatic Control, IEEE Transactions on  (Volume:25 ,  Issue: 3 )