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Guidance of guidance of inertial objects on highly maneuvering targets

Keywords:

V.I. Merkulov


Based on the analysis of existing methods of homing concluded that their low efficiency of interception super- and hypersonic targets, caused by the inertia of the object. On the basis of the mathematical apparatus of the statistical theory of optimal control law a guidance method was synthesized which takes into account dynamic properties of the target and the interceptor. The analysis of the resulting guidance method and its comparison with existing methods are performed.
References:
June 24, 2020
May 29, 2020

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