FIELD: aviation.
SUBSTANCE: group of inventions relates to a method and system for automatic control of thrust in flight, a method of controlling an automatic device of aircraft traction device, a material machine-readable carrier. For automatic traction control in flight, engine control lever position sensor angle is calculated in certain manner, controlling engine control lever to maintain aircraft preferred mode of flight. To control the traction automat, analysis of the received flight impact is performed, traction automaton is actuated in the hold mode to determine that this action will not lead to deviation from the preferable flight state of the aircraft. Material machine-readable medium contains instructions stored thereon to implement said methods. Proposed device comprises sensor to determine flight parameter, processor, electromechanical mechanism to control engine control lever.
EFFECT: proposed automatic control of thrust in flight.
22 cl, 9 dwg
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