FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft control systems. Proposed control system comprises computer (15), engine control device (17) that perform control functions on the basis of thrust control system, drive (16) of control surface (3) to displace control surface on the basis of control surface deflection angle control signal, and control surface fault detector (18). On the case of fault of at least one control surface, computer computes thrust control signal and control surface deflection angle control signal. In compliance with second version, apart from aforesaid means, control system comprises response control filter (23) that adjusts responses of engines and control surfaces.
EFFECT: stable flight.
6 cl, 1 dwg
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