Flight control system for an aircraft

摘要

Flight control system for an aircraft. According to the invention, this control system is characterised in that it comprises a first calculating assembly 21 associated with the ailerons 6, with the elevators 10 and with the variable-incidence horizontal empennage 5 and a second calculating assembly 22, different in origin and design from those of the said first calculating assembly 21 associated with the said deflectors 7 and air brakes 8, as well as with the elevators 10 in the case of a defect in the first calculating assembly 21. <IMAGE>