The invention discloses an aircraft auxiliary driving 
system and method for asymmetric thrust compensation in the approach phase. The 
system includes an asymmetric thrust identification subsystem (100), an auxiliary level decision-making subsystem (200), and an auxiliary compensation control subsystem  (300), an 
autonomous control subsystem (400), and a control coordination 
system (500).  After a single engine failure occurs in a twin-engine aircraft, the lateral balance of the aircraft is destroyed, and the 
yaw moment and sideslip angle continue to increase.  If it occurs during the approach phase that is closer to the ground, the 
pilot needs to make quick decisions and restore a stable approach state, otherwise there will be a risk of crashing.  The invention monitors the state of the engine in real time through the asymmetrical thrust identification subsystem (100).  If a single engine failure occurs, the auxiliary level decision-making subsystem (200) is started, and the auxiliary mode for the 
pilot is given according to the information of the man-
machine environment.  Through the auxiliary compensation control subsystem (300) or the 
autonomous control subsystem (400), the 
rudder surface deflection command is automatically calculated, and input into the aircraft through the control coordination system (500), assisting the 
pilot to complete the approach and landing task, effectively ensuring 
flight safety  .