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
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