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
收藏
页码：428 / 437
页数：10
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