FIELD: armament aids for military aeroplanes, in particular, for multi-mission fighters, applicable for destruction of visible highly maneuvering air targets, as well as for provision an active defense of aeroplanes.
SUBSTANCE: the substance is in determining the angular velocity of the target motion and accomplishing the target designation with taking into account the target attitude and angular velocity. The target motion parameters analysis unit consists of a differentiating circuit, n-threshold device, n-flip-flop, n-first hates, the first adder, the first, second, third delay lines, the second, third and fourth gates the second, third and fourth threshold devices, the first and second shift registers, the first and second NAND circuits, the first and second AND circuit, pulsar, the first second counters, subtracting device, divider, integrator, the second adder, signal selector.
EFFECT: enhanced accuracy of target indication of the missile homing head.
2 dwg
