Adaptive nonlinear robust relative pose control of spacecraft autonomous rendezvous and proximity operations

被引:15
|
作者
Sun, Liang [1 ,3 ]
Huo, Wei [1 ]
Jiao, Zongxia [2 ]
机构
[1] Beihang Univ, Sch Automat Sci & Elect Engn, Res Div Sci & Technol 7, Aircraft Control Lab, Beijing 100191, Peoples R China
[2] Beihang Univ, Sch Automat Sci & Elect Engn, Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R China
[3] Beihang Univ, Res Div 7, Xueyuan Rd 37, Beijing 100191, Peoples R China
基金
中国博士后科学基金; 中国国家自然科学基金;
关键词
Spacecraft control; Rendezvous and proximity; Robust control; Adaptive control; Disturbance attenuation; ATTITUDE-CONTROL; POSITION; TRACKING; SYNCHRONIZATION; DOCKING;
D O I
10.1016/j.isatra.2016.11.022
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper studies relative pose control for a rigid spacecraft with parametric uncertainties approaching to an unknown tumbling target in disturbed space environment. State feedback controllers for relative translation and relative rotation are designed in an adaptive nonlinear robust control framework. The element-wise and norm-wise adaptive laws are utilized to compensate the parametric uncertainties of chaser and target spacecraft, respectively. External disturbances acting on two spacecraft are treated as a lumped and bounded perturbation input for system. To achieve the prescribed disturbance attenuation performance index, feedback gains of controllers are designed by solving linear matrix inequality problems so that lumped disturbance attenuation with respect to the controlled output is ensured in the L(2-)gain sense. Moreover, in the absence of lumped disturbance input, asymptotical convergence of relative pose are proved by using the Lyapunov method. Numerical simulations are performed to show that position tracking and attitude synchronization are accomplished in spite of the presence of couplings and uncertainties. (C) 2016 ISA. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:47 / 55
页数:9
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