FIELD: control; regulation.
SUBSTANCE: group of inventions relates to the method and system of flight control of the aircraft. Flight control system contains two processing units for controlling the drive of the aircraft engine, at least two sensors for each processing unit, and emergency communications. Measurement data of the first sensor and data of the first drive is transmitted to the second processing unit, measurement data of the second sensor and data of the second drive is received from the second processing unit, data about the health of the second processing unit is received, data about the health of the first processing unit is determined, switching of work of blocks depending on indicators of health thereof is provided.
EFFECT: improved resistance to malfunction due to redundancy of processing units and redundancy of communication facilities between them.
10 cl, 5 dwg
