FIELD: instrumentation engineering. SUBSTANCE: device has roll channel and lateral g-load channel. Each channel is provided with subtraction element and summing amplifier. These members form control signals for roll and lateral g-load. Device is provided with sine function forming unit, cosine function forming unit, inverting amplifier, maneuvering jet engine control signal shaper, integrator, non-linear element with dead zone, two limiters, tangent function signal former, two correction function generators, three amplifiers, three multipliers, roll channel output summer, scaler and divider. EFFECT: extended functional capabilities at deficit of aerodynamic control. 5 dwg
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