论文信息 - OPTIMAL EVASIVE MANEUVERS IN CONDITIONS OF UNCERTAINTY

OPTIMAL EVASIVE MANEUVERS IN CONDITIONS OF UNCERTAINTY

Abstract : Optimal missile avoidance by an evader not having information on the relative state is analysed. This problem is equivalent to the homing of a missile of known parameters against a randomly maneuvering target. The objective is to maximize the R.M.S. miss distance by selecting the optimal frequency of a periodical maneuver with random initial phase. Comparison to results of missile avoidance with perfect information shows that the maximized R.M.S. miss distance can reach 60-80% of the optimal deterministic value.

J. Shinar | E. Besner

[1] W. R. Wells,et al. Optimal evasive tactics against a proportional navigation missile with time delay. , 1973 .

[2] Output ensemble average of periodically excited linear time-varying systems , 1980 .

[3] J. E. Kain,et al. Extending the Intercept Range of Tactical Missiles Against Jamming Targets. , 1975 .

[4] J. Shinar. Analysis of three-dimensional optimal evasion with linearized kinematics , 1978 .

[5] R. H. Battin,et al. Random Processes in Automatic Control. , 1957 .

[6] J. Shinar,et al. Analysis of Optimal Evasive Maneuvers Based on a Linearized Two-Dimensional Kinematic Model , 1977 .

[7] C. Desoer,et al. Linear System Theory , 1963 .

[8] E. L. Peterson,et al. Statistical Analysis and Optimization of Systems , 1962 .

[9] J. Shinar,et al. Analysis of Three-Dimensional Optimal Evasion with Linearized Kinematics , 1979 .