second order sliding mode
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2021 ◽  
pp. 743-750
Author(s):  
F. Mazouz ◽  
S. Belkacem ◽  
G. Boukhalfa






2021 ◽  
Author(s):  
Zeyu Guo ◽  
Zuo Wang ◽  
Shihua Li

Abstract 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 towards 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.



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