Aiming at the parameter perturbation and rudder surface faults in supermaneuver flight of thrust vector aircraft, a fault-tolerant control method based on terminal sliding-mode is proposed. Firstly, the rudder surface fault model of thrust vector aircraft is given. Then, the terminal sliding-mode control laws are designed for the attitude angle loop and angle velocity loop respectively, and the projection adaptive law is introduced to estimate and compensate for the parameter perturbation and the rudder surface faults. Finally, the rudder deflection command signal is obtained, and the Lyapunov stability analysis of the system is carried out. The Matlab/Simulink simulation results verify that the proposed fault-tolerant control law can realize the tolerance for parameter perturbation and rudder surface faults of supermaneuver flight, and the adaptive law can accurately estimate the rudder faults.