FIELD: aviation.
SUBSTANCE: invention relates to a method for generating auxiliary control signals on an airplane run. To generate auxiliary signals, control signals from the sensors of the flight parameters measuring system are used, automatic control system of the flight, automatic differential control of the brakes of the wheels and sections of the spoilers on signals from the limit switch and on the speed of unroll of the brake wheels of each main support, determine the extent of the braking of the wheels, control the direction of lateral displacement relative to the axis of the runway.
EFFECT: it is ensured an increase in flight safety during the run after landing in conditions of significant lateral disturbances and control errors.
1 cl, 5 dwg
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