FIELD: aircraft engineering.
SUBSTANCE: proposed system comprises control stick position pickup, first adder, aileron drive and ailerons, second adder, rudder drive and rudder, bank angular speed pickup and yaw angular speed pickup, first pre-filter of control stick position pickup, third adder, first link with insensitivity zone and constriction, second pre-filter, fourth adder, second nonlinear element with insensitivity zone and constriction, first isodromic limiter, second isodromic filter, second limiter and second link with insensitivity zone.
EFFECT: optimum aircraft control.
1 dwg
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