ADRC FRACTIONAL ORDER PID CONTROLLER DESIGN OF HYPERSONIC FLIGHT VEHICLE

作     者：秦昌茂 齐乃明 吕瑞 朱凯 Qin Changmao;Qi Naiming;Lii Rui;Zhu Kai

作者机构：哈尔滨工业大学航天工程与力学系 

出 版 物：《Transactions of Nanjing University of Aeronautics and Astronautics》 (南京航空航天大学学报（英文版）)

年 卷 期：2011年第28卷第3期

页      面：240-245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 Innovation Foundation of Aerospace Science and Technology(CASC200902)~~ 

主　　题：hypersonic flight vehicle active disturbance rejection controller(ADRC) fractional order PID D-decomposition method 

摘      要：Active disturbance rejection controller（ADRC）uses tracking-differentiator（TD）to solve the contradiction between the overshoot and the rapid *** order proportion integral derivative（PID）controller improves the control quality and expands the stable region of the system *** fractional order（ADRFO）PID controller is designed by combining ADRC with the fractional order PID and applied to reentry attitude control of hypersonic *** results show that ADRFO PID controller has better control effect and greater stable region for the strong nonlinear model of hypersonic flight vehicle under the influence of external disturbance,and has stronger robustness against the perturbation in system parameters.