FIELD: aviation.
SUBSTANCE: invention relates to a method for automatic generation of auxiliary signals on a ground section of aircraft motion. To implement the method, control signals of a system of sensors are used, with the help of which auxiliary control signals are generated in the calculator for the brake drive of the main landing gear struts, a drive of the interceptor sections, a control drive for turning the nose wheels. Generation of auxiliary control signals is carried out in a step-by-step manner.
EFFECT: higher efficiency of control actions on elements of aircraft control system at take-off if it is necessary to perform interrupted take-off and landing when running in conditions of loss of controllability or threat of side rolling of aircraft beyond runway.
1 cl, 20 dwg
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