FIELD: aviation.
SUBSTANCE: group of inventions relates to a system, a method for automatic flight protection and a method of protecting an aircraft structure parameter. Proposed system comprises dynamic pressure sensor, processor and control surface to limit wing lift coefficient. Maximum value of angle of attack depending on dynamic pressure is used to protect parameter of aircraft structure. For automatic flight protection, determining or obtaining dynamic pressure or aircraft speed, using the processor based on the dynamic pressure, the wing lift coefficient is automatically limited.
EFFECT: providing automatic control of wing lifting force for flight control.
19 cl, 13 dwg
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