Attitude Quaternion Control in the Final Approach Phase of Rendezvous and Docking by Sliding Mode Control

被引：0

作者：

Zong Xiaoxiao ^{[1
]}

Liu Zhenghua ^{[1
]}

Ren Yan ^{[1
]}

Li Nan ^{[2
]}

机构：

[1] Beihang Univ, Sch Automat Sci & Elect Engn, Beijing, Peoples R China

[2] Beihang Univ, Sch Astronaut, Beijing, Peoples R China

来源：

PROCEEDINGS OF THE 10TH WORLD CONGRESS ON INTELLIGENT CONTROL AND AUTOMATION (WCICA 2012) | 2012年

关键词：

rendezvous and docking; attitude control; attitude quaternion; sliding mode control; SYSTEMS;

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

For the relative attitude control problem in phasing period of rendezvous and docking, attitude quaternion was adopted to describe the dynamic model and the kinematics equation of spacecraft. Then attitude quaternion PD feedback was designed to control the relative attitude successfully. On this basis, the sliding mode control was researched and used in relative attitude control to improve accuracy and build up anti-jamming ability. The simulation results demonstrate that sliding mode controller is more superior in rapidity and robustness.

引用

页码：2177 / 2181

页数：5

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