Dynamic surface control and active disturbance rejection control-based integrated guidance and control design and simulation for hypersonic reentry missile

作     者：Cong Zhang Yun-Jie Wu 

作者机构：State Key Laboratory of Virtual Reality Technology and Systems Beihang UniversityBeijing 100191P.R.China School of Automation Science and Electrical Engineering Beihang UniversityBeijing 100191P.R.China Science and Technology on Aircraft Control Laboratory Beihang UniversityBeijing 100191P.R.China 

出 版 物：《International Journal of Modeling, Simulation, and Scientific Computing》 (建模、仿真和科学计算国际期刊（英文）)

年 卷 期：2016年第7卷第3期

页      面：216-242页

核心收录：

学科分类：08[工学] 081101[工学-控制理论与控制工程] 0811[工学-控制科学与工程] 081102[工学-检测技术与自动化装置] 

基　　金：funded in part by the National Natural Science Foundation of China under Grant 91216304 

主　　题：Hypersonic reentry missile integrated guidance and control dynamic surface control active disturbance rejection control simulation 

摘      要：This paper proposes a novel integrated guidance and control(IGC)method combining dynamic surface control(DSC)and active disturbance rejection control(ADRC)for the guidance and control system of hypersonic reentry missile(HRM)with bounded ***,the model of HRM is ***,the proposed IGC method based on DSC and ADRC is *** stability of closed-loop system is proved *** is worth mentioning that the ADRC technique is used to estimate and compensate the disturbance in the proposed IGC *** makes the closed-loop system a better performance and reduces the chattering caused by lumped ***,a series of simulations and comparisons with a 6-DOF non-linear missile that includes all aerodynamic effects are demonstrated to illustrate the effectiveness and advantage of the proposed IGC method.