FIELD: aviation; guidance systems.
SUBSTANCE: invention is intended for interception of aerial object at large distances, including intensive maneuvering one. For this purpose, combined guidance of AC is implemented at operation of information-computer system (ICS) in three modes: target designation, radio command guidance (RCG) and homing. At that, all-sector intercept of aerial object is ensured irrespective of operating mode, and ICS operation algorithms are robust to change of modes. For this used optimal algorithms for AC control in modes of remote guidance and homing, synthesised based on use of system analysis and methods of automatic control theory, AC guidance systems theory, evaluation theory, optimum control stochastic theory, mathematical apparatus for solving differential equations, vector analysis and matrix algebra principles.
EFFECT: broader functional capabilities.
1 cl, 6 dwg
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