FIELD: control systems.
SUBSTANCE: group of inventions relates to aircraft electrical control system and method of its control. Electric steering system comprises electric motor for steering, control module for supply of energy to electric element of aircraft. To control electric steering system, electric motor is rotated, which is intended for aircraft steering in order to apply braking force to wheel and generate recuperative energy according to this force, transmitting the recuperative energy to the electric element of the aircraft for its actuation for landing or re-take-off after landing cancellation.
EFFECT: higher efficiency of recuperative energy use.
9 cl, 3 dwg
