FIELD: instrumentation engineering; onboard automatic control systems for flying vehicles of aeroplane configuration.
SUBSTANCE: proposed control system includes control process parameter setters, two multiplexers, two modulus detection units, two positive polarity signal detection units, two relay elements, two comparison units, two summing-up amplifiers, AND gate, controllable selector switch, four limiters, pitch and roll angle sensors, pitch and roll rate sensors, two adders and two actuating units.
EFFECT: enhanced accuracy of control due to combination method of guidance of unmanned flying vehicle.
1 dwg
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