FIELD: aircraft engineering.
SUBSTANCE: invention relates to onboard remote control systems. Proposed system comprises the following functional units, i.e. algorithm reconfiguration unit, unit to generate signals converting control conditions into message generation, unit to compute dynamic factors, input signal filtration unit. It comprises also αfloor-function activation unit, autopilot cutout signal generation unit, elevator rudder control unit, tailplane control unit, rudder control unit, multi-function spoiler, drag flap control unit and wing high-lift devices. System maintains relative position of flaps and slats in compliance with the fixed positions of control stick handle and protects wing high-lift devices against excessive loads.
EFFECT: protection of controlled parametres against overloads; switching on maximum operating conditions in approximating to stall angles; limiting angle of attack, maximum and minimum overload na and negative pitch angle; protection fuselage tail against impacts on runway in taking off; control over flight conditions without interference of pilot.
2 cl, 6 dwg
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