FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly, to manual control systems in course channel of aircraft of normal configuration with differentially deflected stabilizer. In the control system, an additional cross-link circuit is formed, which deflects the rudder by a value sufficient to reduce the slip angles and lateral overload occurring at the considered form of movement to an acceptable level. This algorithm takes into account both flight mode parameters: number M, altitude (static pressure), angle of attack, and position (deflection angle) of the stabilizer during control in the longitudinal plane and the angle of deflection of the brake flap.
EFFECT: control system makes it possible to reduce overshoot of lateral overload approximately by two times to values acceptable as per pilot estimation.
1 cl, 3 dwg
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