FIELD: aviation; flying vehicles provided with high-lift devices. SUBSTANCE: control system is additionally provided with second limit switch of landing gear located between second output and vertical velocity setter and second input of safe speed computer unit and with second computer unit and third limit switch of landing gear located between safe speed computer unit and amplifier and connected in series. EFFECT: automatic control of wing high-lift devices at take-off and considerable reduction of danger of overrun of flying vehicle in case of failure of engine during take-off run. 1 dwg
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