Output Feedback Stabilization of Spacecraft Autonomous Rendezvous Subject to Actuator Saturation

被引：0

作者：

Qian Wang ^{[1
]}

Guang-Ren Duan ^{[1
]}

机构：

[1] Center for Control Theory and Guidance Technology, Harbin Institute of Technology

来源：

International Journal of Automation and Computing | 2016年 / 13卷 / 05期

基金：

中国国家自然科学基金;

关键词：

Dynamic gain scheduling; output feedback; parametric Lyapunov equation; input saturation; spacecraft rendezvous;

D O I：

暂无

中图分类号：

V448.2 [航天器制导与控制];

学科分类号：

081105 ;

摘要：

This paper studies the output feedback dynamic gain scheduled control for stabilizing a spacecraft rendezvous system subject to actuator saturation. By using the parametric Lyapunov equation and the gain scheduling technique, a new observer-based output feedback controller is proposed to solve the semi-global stabilization problem for spacecraft rendezvous system with actuator saturation. By scheduling the design parameter online, the convergence rates of the closed-loop system are improved. Numerical simulations show the effectiveness of the proposed approaches.

引用

页码：428 / 437

页数：10

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