FIELD: aviation.
SUBSTANCE: control system of manned aircraft (AC) with adaptive cross-coupling comprises a roll control position of aircraft control knob (ACK), roll angular velocity sensor, air signals system, three noise suppression filters, boost filter, pedal position sensor, angular velocity sensor by angular yaw rate, linear acceleration sensor in side plane of aircraft movement, sensor of angles of attack and sliding, seven scaling units, rudder drives of ailerons and rudder, two adder, position transmitter of pitch-by-pitch, three non-linear correcting units, three signal multiplication units connected in certain manner.
EFFECT: ensuring satisfactory controllability of manned aircraft by roll in the entire range of allowable angles of attack when performing arbitrary spatial manoeuvres.
4 cl, 5 dwg
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