Control law design of aircraft super-maneuverable flight based on dynamic surface backstepping control

It proposed a dynamic surface backstepping control for super-maneuverable flight. In contrast to the basic backstepping method, our scheme abandons the adaptive laws, and introduces sliding surfaces and reaching conditions to design the virtual control signal and the final control signal. Furthermore, instead of involving model differentiation, a low pass dynamic filter is used in the two steps backstepping design, which provides a more simplified control algorithm. The simulation results show that the new scheme achieves a simple design procedure and a satisfying tracking performance.