The Kinematics and Control of Relative Attitude Pointing for Spacecraft Formation Flying

被引：0
|
作者：
Gao, YouTao [1 ]
Xu, Bo [2 ]
Lu, YuPing [1 ,2 ]
机构：
[1] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing 210016, Jiangsu, Peoples R China
[2] Nanjing Univ Aeronaut & Astronaut, Coll Astronaut, Nanjing 210016, Jiangsu, Peoples R China
来源：
CCDC 2009: 21ST CHINESE CONTROL AND DECISION CONFERENCE, VOLS 1-6, PROCEEDINGS | 2009年
基金：
国家高技术研究发展计划(863计划);
关键词：
Spacecraft Formation Flying; Coupled Control; Attitude pointing Kinematics and Dynamics; Sliding Mode Control; TRACKING;
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：
A geometric method which exploits the coupled relationship between relative position and relative attitude pointing is proposed to derive the desired relative attitude pointing Euler angles. The coupled kinematics and the dynamics equations of the relative attitude pointing are obtained. A sliding mode control based on exponent reaching law is applied to the coupled control system. The simulation results show the effectiveness of the coupled control system on the relative attitude pointing and relative position of spacecraft formation flying.
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页码：280 / +
页数：2
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