Saturated output feedback control for finite-time attitude stabilization of spacecraft

Author:

Xia Yuquan1ORCID,Su Yuxin1ORCID

Affiliation:

1. School of Electro-Mechanical Engineering, Xidian University, Xian, China

Abstract

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.

Publisher

SAGE Publications

Subject

Mechanical Engineering

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