In view of control on high angle-of-attack maneuvering flight of aircraft with thrust vector, this study mainly focuses on strategy of fused control of thrust vector with aerodynamic control surface. Thrust vector makes fight control surfaces appear redundant, which needs a reasonable allocation to manipulate deflection to obtain satisfactory stability and maneuverability. Based on the chain combination and cascade structure, combined with Anti-Windup anti-saturation combination strategy, the thrust vector/aero rudder integration methods which include Anti-Windup feedback thrust vector control was proposed. The form of thrust vectoring control structure and the performance advantages of aircraft with thrust vectoring were studied, the benefits of thrust vector control technology as well as the impact of response characteristics were analyzed. The result of stimulation shows that Anti-Windup control surface integration control structure designed has remarkably better performance and the merits of rapid response speed, minor model tracking error and better characteristic.