Attitude Regulation With Bounded Control in the Presence of Large Disturbances With Bounded Moving Average

被引:0
|
作者
Li, Ang [1 ,2 ]
Astolfi, Alessandro [2 ,3 ]
Liu, Ming [1 ]
机构
[1] Harbin Inst Technol, Sch Astronaut, Harbin 150080, Peoples R China
[2] Imperial Coll London, Dept Elect & Elect Engn, London SW7 2AZ, England
[3] Univ Roma Tor Vergata, Dipartimento Ingn Civile & Ingn Informat, I-00133 Rome, Italy
基金
中国国家自然科学基金;
关键词
Bounded control; cubeSats; robust attitude regulation; ultimate boundedness;
D O I
10.1109/JAS.2022.105557
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
The attitude regulation problem with bounded control for a class of satellites in the presence of large disturbances, with bounded moving average, is solved using a Lyapunov-like design. The analysis and design approaches are introduced in the case in which the underlying system is an integrator and are then applied to the satellite attitude regulation problem. The performance of the resulting closed-loop systems are studied in detail and it is shown that trajectories are ultimately bounded despite the effect of the persistent disturbance. Simulation results on a model of a small satellite subject to large, but bounded in moving average, disturbances are presented.
引用
收藏
页码:834 / 846
页数:13
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