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It is important for reconfiguration control in the presence of control surface failure as it will influence the flight safety of the aircraft. Considered the characteristic of the control surface failure, L1 adaptive reconfiguration control method is proposed. Firstly, according to control surface failure impacting the aerodynamic parameter, the failure model is built. Then, based on of adaptive and robust characteristics, the adaptive law and filter are chose in order to design controller. Finally, Simulation on the elevator failure aircraft shows the reconfigurable control operates well.