FIELD: aviation.
SUBSTANCE: invention relates to the unmanned aerial vehicles control method. To this end, generating and transmitting control signals from the command station to the aircraft using the communication means complex, interacting along the five communication lines with the onboard digital computer, by means of which check of landing gear supports is checked and analysis of information on conditions of onboard systems, communication lines and command station, and at failure detection of at least one onboard system or at least three communication lines, or command station. In the absence of reduction of chassis supports, return and landing are performed, and in the presence of reduction of landing gear supports, and if the instrument speed is less than the speed of decision making, the takeoff run is stopped.
EFFECT: higher flight safety.
3 cl, 3 dwg
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