Terminal Sliding Mode Control for Cyber Physical System Based on Filtering Backstepping

作     者：Fei Li Jian-Bo Hu Lei Zheng Jian-Hao Wang 

作者机构：Equipment Management and Safety Engineering College Air Force Engineering University Unit 93286People's Liberation Army 

出 版 物：《International Journal of Automation and computing》 (国际自动化与计算杂志（英文版）)

年 卷 期：2015年第12卷第5期

页      面：497-502页

核心收录：

学科分类：08[工学] 081105[工学-导航、制导与控制] 0811[工学-控制科学与工程] 

基　　金：supported by the State Key Laboratory of Industrial Control Technology Zhejiang University China(No.ICT1447) Shanghai Leading Academic Discipline Project(No.J50103) 

主　　题：Cyber-physical system(CPS) disturbance uncertainti 

摘      要：Based on a nonlinear flight dynamic model with aerodynamic coefficients and external disturbance uncertainties, which is a typical cyber physical system, a filtering backstepping terminal sliding mode control method is proposed for a robust *** tracking differentiator can provide the capability of solving the problem of complexity explosion in backstepping controllers to simplify the backstepping implementation. Nonlinear disturbance observers are used to observe the uncertainties of the nonlinear flight dynamic system. The terminal sliding mode controller is designed to improve its convergence rate and the tracking accuracy. Finally,nonlinear 6-degree-of-freedom simulation results for an F-16 aircraft model elaborate the effectiveness of the proposed control system.