FIELD: aircraft engineering.
SUBSTANCE: group of inventions relates to aircraft control, method for identifying potential stalling state, and stall control system. During aircraft control identified are angle of attack, coefficient of lift, air speed for emergency warning for aircraft in a certain manner. To indicate potential stalling state for aircraft during flight, lift coefficient is identified for emergency warning, and it is adjusted in response to number of changes in current state of aircraft, set of threshold values is identified for generation of emergency warning for aircraft operator. System for stall controlling comprises generator of threshold values, configured to identify critical values for emergency warning.
EFFECT: provision of emergency warning in critical flight conditions is allowed.
20 cl, 14 dwg
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