Super-Maneuver Flight control design using constrained adaptive backstepping and sliding mode

Super-maneuver flight control is designed based on constrained backstepping and second-order sliding mode. A sort of MIMO second order sliding mode algorithm is designed. The main advantages of the Super-Maneuver flight control law combined backstepping and second order sliding mode are the prevention of chattering, higher accuracy and a significant simplification of the control law. The results of super-maneuver flight simulation show that the system achieves high dynamic and static performance and robustness.