FIELD: aeronautical engineering; aircraft engine air intake control system. SUBSTANCE: aircraft engine air intake control system includes correcting device with adder and altimeter, engine specific revolutions shaping unit, program compiler, program correction inhibit unit, program corrector and air intake panel motion drive. program compiler is connected with air intake panel motion drive; output of air intake panel motion drive is connected via feedback unit to program compiler. Altimeter is connected to adder. ON/OFF command unit includes transducers connected with adder. Adder output is connected with input of program correction inhibit unit which is connected in its turn with program corrector. Program corrector is connected with engine specific revolutions shaping unit and with program compiler. EFFECT: improved characteristics of air in take for aircraft with delta wings and horizontal nose plane. 3 dwg
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