FIELD: aircraft engineering.
SUBSTANCE: group of inventions relates to aircraft, method and device for aircraft control device power feedback control. Device for control device active power feedback control has computer, position sensor, drive. For control device active power feedback control, control device is moved using computer controlled drive, control device current position is measured, setting current entering drive modulation is performed, saturation limit is formed in a certain manner, by means of which setpoint current is saturated by upper and lower limits. Aircraft comprises control unit, control device, control device of active power feedback control device.
EFFECT: higher reliability, accuracy and flexibility of mini control wheel control system.
10 cl, 5 dwg
