Full-state prescribed performance pose tracking of space proximity operations with input saturation

被引:7
作者
Wang, Jun [1 ]
Sun, Liang [1 ,2 ]
Jiang, Jingjing [3 ]
机构
[1] Univ Sci & Technol Beijing, Sch Automat & Elect Engn, Minist Educ, Key Lab Knowledge Automat Ind Proc, Beijing, Peoples R China
[2] Univ Sci & Technol Beijing, Inst Artificial Intelligence, Beijing, Peoples R China
[3] Loughborough Univ, Dept Aeronaut & Automot Engn, Loughborough, Leics, England
基金
中国国家自然科学基金;
关键词
control input saturation; full-state constraint; nonlinear disturbance observer; prescribed performance; spacecraft control; FAULT-TOLERANT CONTROL; ROBUST ADAPTIVE-CONTROL; ATTITUDE-CONTROL; SYSTEMS; DOCKING; STABILIZATION; CONTROLLER; TRANSIENT; DESIGN;
D O I
10.1002/asjc.2929
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 investigates the relative position tracking and attitude synchronization control for spacecraft close-range proximity missions with input saturation and model uncertainties. A robust saturated relative motion controller is proposed for this purpose. Prescribed performance functions are designed to guarantee the transient and steady-state response of the system and the full-state constraints. Then, a nonlinear disturbance observer is developed to estimate the lumped disturbance that comprises the effects of parametric uncertainties and kinematic couplings. At the same time, a linear compensator system is incorporated into the controller design to deal with the control input saturation. Finally, it can be proved via the Lyapunov theory that the closed-loop system is uniformly ultimately bounded stable. Simulation results on the spacecraft close-range rendezvous and docking mission validate the effectiveness of the proposed control approach.
引用
收藏
页码:1350 / 1364
页数:15
相关论文
共 44 条
[1]   Adaptive controller design for spacecraft formation flying using sliding mode controller and neural networks [J].
Bae, Jonghee ;
Kim, Youdan .
JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS, 2012, 349 (02) :578-603
[2]   Robust Adaptive Control of Feedback Linearizable MIMO Nonlinear Systems With Prescribed Performance [J].
Bechlioulis, Charalampos P. ;
Rovithakis, George A. .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 2008, 53 (09) :2090-2099
[3]   A low-complexity global approximation-free control scheme with prescribed performance for unknown pure feedback systems [J].
Bechlioulis, Charalampos P. ;
Rovithakis, George A. .
AUTOMATICA, 2014, 50 (04) :1217-1226
[4]   Robust adaptive variable structure control of spacecraft under control input saturation [J].
Boskovic, JD ;
Li, SM ;
Mehra, RK .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2001, 24 (01) :14-22
[5]   Disturbance observer based control for nonlinear systems [J].
Chen, WH .
IEEE-ASME TRANSACTIONS ON MECHATRONICS, 2004, 9 (04) :706-710
[6]   Asymptotic Tracking Controller Design for Nonlinear Systems With Guaranteed Performance [J].
Fan, Bo ;
Yang, Qinmin ;
Jagannathan, Sarangapani ;
Sun, Youxian .
IEEE TRANSACTIONS ON CYBERNETICS, 2018, 48 (07) :2001-2011
[7]   Robust integrated translational and rotational control for spacecraft rendezvous in unstructured environments [J].
Feng, Zhang .
TRANSACTIONS OF THE INSTITUTE OF MEASUREMENT AND CONTROL, 2018, 40 (11) :3293-3313
[8]   Robust neural-network-based quasi-sliding-mode control for spacecraft-attitude maneuvering with prescribed performance [J].
Fu, Jingbo ;
Liu, Ming ;
Cao, Xibin ;
Li, Ang .
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 112
[9]   History of Space Shuttle rendezvous and proximity operations [J].
Goodman, John L. .
JOURNAL OF SPACECRAFT AND ROCKETS, 2006, 43 (05) :944-959
[10]   Hybrid Global Finite-Time Dual-Quaternion Observer and Controller for Velocity-Free Spacecraft Pose Tracking [J].
Gui, Haichao ;
Wang, Yong ;
Su, Wenjie .
IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2021, 29 (05) :2129-2141