I. Introduction
The Direct-Drive Valve systems are one of the main components which affect the system output performance of the aerospace servo system significantly, which have wide applications in many control fields [1]–[4]. An electrical servo motor of direct drive valve (DDV) is employed to eliminate the disadvantages of the system high sensitivity to oil-contamination and complicated structure, which provides good control output performance. Thus, a host of advanced control strategies have been captured more attention in recent years. As we know, the PID control schemes are by far the most widely employed in industrial control applications, due to its popularity stems from its easy operation, simple system structure and applicability in a wide variety of operating [5], [6], [14], [21], [22]. When the system exists complex, time-varying and some large disturbances, traditional PID control scheme cannot realize the consistent control performance [5], [6].