Title :
On the optimal pure strategy sets for a mixed missile guidance law synthesis
Author :
Shinar, J. ; Forte, I.
Author_Institution :
Fac. of Aerosp. Eng., Technion, Haifa, Israel
fDate :
11/1/1991 12:00:00 AM
Abstract :
The terminal phase of a missile-versus-aircraft engagement in a noise-corrupted environment is formulated as an imperfect information zero-sum differential game. The payoff of the game is the single shot kill probability of the missile to be maximized by its designer and minimized by the pilot of the evading aircraft. In the past, it was shown that in such a game the optimal strategy of the evader is mixed. The proposed formulation allows a mixed strategy for the pursuer. The mathematical basis for such an analysis is provided, and a constructive methodology for the synthesis of missile guidance laws based on the concept of mixed strategies is outlined
Keywords :
game theory; missiles; optimisation; game theory; missile guidance law synthesis; missile-versus-aircraft engagement; noise-corrupted environment; optimisation; pursuit evasion game; single shot kill probability; zero-sum differential game; Aircraft; Automatic control; Control systems; Feedback; Missiles; Nonlinear control systems; Nonlinear systems; Optimal control; Sliding mode control; Variable structure systems;
Journal_Title :
Automatic Control, IEEE Transactions on