Global finite‐time stabilization of a class of perturbed planar systems with actuator saturation and disturbances

2021 ◽  
Author(s):  
Yuxin Su ◽  
Chunhong Zheng ◽  
Paolo Mercorelli
Author(s):  
Yuquan Xia ◽  
Yuxin Su

The finite-time attitude stabilization of spacecraft subject to actuator constraints and attitude measurements only is investigated. A saturated output feedback finite-time proportional-derivative control is proposed. Lyapunov stability theory and homogeneous method are employed to show the finite-time stabilization. Advantages of the proposed control include the finite-time stabilization featuring faster transient and higher precision and the absence of the modelling information and the velocity measurements in the control law formulation, and thus, it offers an easy-going solution for high-quality motion control of spacecraft. An additive feature is that the actuator saturation will not be reached by selecting the control gains a priori. Simulations are presented to illustrate the effectiveness of the proposed control.


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