To reduce the effect of hysteresis of piezoceramic actuator to the accuracy of the nano positioning stage,inverse Preisach model is used to compensate the hysteresis nonlinearity and an adaptive sliding mode controller is designed to cancel the remaining hysteresis,uncertainty of the model,and other disturbances.

A missile reaction-jet/aerodynamic compound control system design method based on adaptive sliding mode control (ASMC) and fuzzy logic is proposed.

Aiming at the tracking control problem of electrohydraulic position servo systems,a design method of adaptive sliding mode control with parameter adaptive performances,was presented based on sliding mode control theory.

By adopting playback control approach,the stability of the entire system state was guaranteed,then,to eliminate the uncertainties and external disturbance in the system,an integrated adaptive sliding-mode controller was designed.

They are exploited respectively to force system to move along sliding mode surface,to eliminate known disturbance to linear nominal system,to overcome uncertain disturbance(using fuzzy sliding mode adaptive control without known uncertain bound).

An adaptive fuzzy sliding mode control (AFSMC) method was used to design the moving mass control systems for the pitch and yaw channels to overcome the effects of the coupled terms and to improve the robustness and control precision of the moving mass control systems.