FIELD: aviation.
SUBSTANCE: invention relates to method for formation of astatic high-speed dampers of aircrafts. To implement method in each control channel required aircraft angular velocity value is set, angular velocity of the aircraft is measured, and a signal is generated on the steering drive, which is obtained by forming and processing two additional signals in a certain way based on the mathematical model of the aircraft motion, the specified and measured angular velocity of the aircraft.
EFFECT: higher efficiency of dampers and stability of aircraft.
1 cl, 4 dwg
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