Application Research on Time optimal Synthesis Function for Missile Eiectromechanical Actuator Control System
The closed-loop system using time optimal synthesis function has characteristics of fast convergence and no buffeting. This paper brings forward a new electromechanical actuator control system which uses time optimal synthesis function to complete the design of control law and nonlinear state tracking feedback. The simulation results and experiments on motor servo loading system show that the controller has good dynamic performance, little steady-state error, and strong robust for uncertainty of parameters and changes in external load.
the time optimal Synthesis Function Control Law Nonlinear State tracking feedback digital electromechanical actuator robust
Yang Yao Wang Mingang Li Qiang Zhao Gang
The School of Astronautics Northwestern Polytechnical University Xian 710072 PR Shaan Xi China
国际会议
长沙
英文
675-678
2010-03-13(万方平台首次上网日期,不代表论文的发表时间)