Spacecraft formation-containment flying control with time-varying translational velocity

作     者：Liangming CHEN Chuanjiang LI Yanning GUO Guangfu MA Baolong ZHU Liangming CHEN;Chuanjiang LI;Yanning GUO;Guangfu MA;Baolong ZHU

作者机构：Department of Control Science and EngineeringHarbin Institute of TechnologyHarbin 150001China School of Electrical Engineering and AutomationQilu University of Technology(Shandong Academy of Sciences)Jinan 250353China 

出 版 物：《Chinese Journal of Aeronautics》 (中国航空学报（英文版）)

年 卷 期：2020年第33卷第1期

页      面：271-281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 National Natural Science Foundation of China(Nos.61876050 61673135 61603114) 

主　　题：Adaptive gain technique Distributed control Formation-containment Formation control Spacecraft formation flying 

摘      要：This paper investigates the problem of Spacecraft Formation-Containment Flying Control(SFCFC)when the desired translational velocity is *** SFCFC problem,there are multiple leader spacecraft and multiple follower spacecraft and SFCFC can be divided into leader spacecraft’s formation control and follower spacecraft’s containment ***,under the condition that only a part of leader spacecraft can have access to the desired time-varying translational velocity,a velocity estimator is designed for each leader ***,based on the estimated translational velocity,a distributed formation control algorithm is designed for leader spacecraft to achieve the desired formation and move with the desired translational velocity ***,to ensure all follower spacecraft converge to the convex hull formed by the leader spacecraft,a distributed containment control algorithm is designed for follower ***,to reduce the dependence of the designed control algorithms on the graph information and increase system robustness,the control gains are changing adaptively and the parametric uncertainties are handled,***,simulation results are provided to illustrate the effectiveness of the theoretical results.