A dynamic inversion control method of super maneuverable aircraft is studiedwhich is based on sliding mode observer using Super twisting algorithm and PI.Firstlyanalysis is made to the super maneuvering aircrafts nonlinear characteristic with consideration of the thrust vectorand a nonlinear simulation platform of the aircraft is established.In the fast loopthe direct external disturbance torque is estimated using sliding mode observer of Super twisting algorithm and then the compensation control law is designed for interference suppression.In the slow loopthe classical PI control is used to offset the system inversion error caused by the nonlinear cancellation.Finallythe control law is used in the cobra maneuver of large angle of attack.The simulation shows that the designed control law can make the super maneuverable aircraft have a good rapidity and stability.