Abstract
The flying quality of an aircraft is jointly determined by its aerodynamic performance and flight control system. The manual flight control system of large transport aircraft is generally composed of the fly-by-wire flight control system and machinery control system. The fly-by-wire flight control system generally has a normal working mode, degraded working mode, simulated backup working mode, and direct chain working mode. The machinery control system is only an important supplement to ensure the safety of the aircraft. With the progress of technology and the continuous improvement of the reliability of fly-by-wire flight control system, modern aircraft have gradually phased out the machinery control system, such as A380, A400M, and B787 aircraft.
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