Based on the measurement information of the seeker,adaptive sliding-mode guidance was designed for the interceptor against maneuvering targets in low-altitude atmosphere and a method to eliminate the flutter was given by using fuzzy control theory.

In order to overcome the shortcomings of traditional guidance law,a new adaptive sliding mode guidance law based on the design of the adaptive sliding mode guidance law was proposed.

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.