共 44 条
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.
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页码:1350 / 1364
页数:15
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