Adaptive High Maneuvers Flight Control via Improved Dynamic Surface Control Technique

In this paper, an adaptive control method based on improved dynamic surface control (DSC) technique is proposed for a class of high maneuver flight control problems with input saturation and dead zone input. By designing adaptive disturbance compensation terms, the influences caused by external disturbances, modeling errors and uncertainties such as aerodynamic parameters have been suppressed effectively, which has a strong anti-jamming capacity. Because of the application of the improved dynamic surface technique, the control method not only reduces the computational burden of the control design, but also guarantees the global uniformly ultimately boundedness (GUUB) of all the signals in the closed-loop system.