Global finite-time set stabilization of spacecraft attitude with disturbances using second-order sliding mode control

被引：0
|
作者：
Zeyu, Guo [1 ,2 ]
Zuo, Wang [1 ,2 ]
Shihua, Li [1 ,2 ]
机构：
[1] Southeast Univ, Sch Automat, Nanjing 210096, Peoples R China
[2] Minist Educ, Key Lab Measurement & Control Complex Syst Engn, Nanjing 210096, Peoples R China
来源：
NONLINEAR DYNAMICS | 2022年 / 108卷 / 02期
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; Attitude stabilization; Global finite-time stability; Second-order sliding mode; Bounded disturbances; RIGID SPACECRAFT; FLEXIBLE SPACECRAFT; TRACKING CONTROL; CONTROL DESIGN; FEEDBACK; STABILITY; OBSERVER;
D O I：
10.1007/s11071-022-07245-5
中图分类号：
TH [机械、仪表工业];
学科分类号：
0802 ;
摘要：
The performance of attitude stabilization control algorithms for rigid spacecraft can be limited by disturbances. In this paper, the global finite-time attitude stabilization problem with disturbances is investigated and handled by constructing a second-order sliding mode controller. Firstly, a virtual controller based on set stabilization idea is constructed to globally finite-time stabilize the system. Then, a relay polynomial second-order sliding mode controller is constructed to guarantee that the tracking error toward the virtual controller will converge to zero in finite-time. Finite-time Lyapunov theory is applied to support the proof and stability analysis. The global finite-time stability holds even with bounded disturbances. The effectiveness and feasibility of the controller are illustrated by the numerical simulations.
引用
收藏
页码：1305 / 1318
页数：14
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