FIELD: aeronautical engineering. SUBSTANCE: connected to force transducer 6 in parallel with control lever 1 is spring-loaded negative stiffness device 8; loading gradient ensured by electrical distance channel is equal to sum of loading gradient of control lever and gradient of spring-loaded negative stiffness device which is made of spring 9 and bell crank 10 articulated together whose axes coincide at neutral position of lever; force applied to spring at negative position is maximum. EFFECT: enhanced stability of system at small loading gradients of control lever. 2 cl, 2 dwg
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