FIELD: aeronautical engineering. SUBSTANCE: flying vehicle remote control system has side control stick 1, banking control action sensor 2 and pitching control action sensor 3, nonlinear units 4 and 5, type "dead zone" in roll channel and pitch channel, flying vehicle motion parameter sensor unit 6, control signal shaping unit 7, actuators 9 of control members 10, as well as functional unit 8 including nonlinear module separation unit, scaling unit, adder and constant signal setter. EFFECT: enhanced accuracy of piloting at simultaneous control in rolling and pitching. 1 dwg
