FIELD: rocketry, applicable in development of TV guidance systems of guided missiles. SUBSTANCE: the system has a device for measurement of range and target angular co-ordinates, device for measurement of range and missile angular co-ordinates, command generating device, unit for forming of program function approximately equal to the missile tangential acceleration, three adders, two amplifiers and two integrators. EFFECT: enhanced accuracy and noise immunity of the TV guidance system, which is attained due to the filtering of the signal of measured range to the missile and computation of static evaluations of range and missile velocity. 1 dwg
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