FIELD: aviation.
SUBSTANCE: invention relates to a method for generating auxiliary control signals on an airplane run. To implement the method, control signals are transmitted from sensors of the flight parameters measurement system to the automatic flight control computer system to generate an auxiliary control signal to the interceptor sections drive, as well as differential control of wheel brakes in certain manner.
EFFECT: higher safety of aircraft motion in conditions of run, reduced load on nasal wheels and damping strut of chassis.
1 cl, 7 dwg
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