FIELD: aircraft.
SUBSTANCE: invention relates to a method for controlling an aircraft during combat maneuvering. To control the aircraft, the parameters of the aircraft's own state vector are determined, the parameters characterizing the position of the controls are determined and their correspondence to the self-state vector and the flight mode is analyzed, the probability of erroneous actions of the crew is calculated and the probability of death of the crew and the aircraft is specified. In case of a catastrophic situation, they give a signal to rescue the crew. In other cases, control actions are formed on the executive systems, ensuring the elimination of special situations.
EFFECT: improved aircraft flight safety.
1 cl, 1 dwg
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