FIELD: instrument making.
SUBSTANCE: invention can be used in guidance systems, namely in self-guidance systems of aircrafts to hypersonic air targets. In addition, there measured and evaluated is angular speed of observing line of hypersonic air target, transverse accelerations of hypersonic air targets and aircraft in horizontal and vertical planes, on the basis of functional conversion of which the aircraft control signal is shaped.
EFFECT: enlarging functional capabilities.
3 dwg
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