中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Comparison of two linearization methods for optimal attitude maneuver of a non-linear flexible spacecraft

文献类型:期刊论文

作者Zheng, J. H.
刊名Ima Journal of Mathematical Control and Information
出版日期2006
卷号23期号:2页码:127-136
关键词non-linear flexible spacecraft optimal attitude maneuver vibration suppression control recursive approximating sequence approach linearization method small sphere approximating approach linearization method stabilization systems
ISSN号0265-0754
通讯作者北京8701信箱
英文摘要In this paper, we consider the optimal attitude maneuver design for a non-linear flexible spacecraft with vibrating solar arrays. Two different linearization methods for the non-linear system are compared in this study. One is the recursive approximating sequence approach (RASA) to design a time-varying linear quadratic regulator (LQR) for the non-linear system and the other is to design a LQR by linearizing the non-linear system at each locally 'frozen' state in any sufficient small sphere along the trajectory. Numerical simulation shows that the later approach gives good design results quickly by scanning the time axis only one time. The RASA method may scan the time axis several times to get a good approach. Moreover, both linearization methods give satisfying control results in attitude maneuver and vibration suppression control for the non-linear flexible spacecraft.
学科主题空间技术
收录类别SCI
原文出处http://imamci.oxfordjournals.org/cgi/reprint/23/2/127.pdf
语种英语
源URL[http://ir.cssar.ac.cn/handle/122/641]  
专题国家空间科学中心_空间技术部
推荐引用方式
GB/T 7714
Zheng, J. H.. Comparison of two linearization methods for optimal attitude maneuver of a non-linear flexible spacecraft[J]. Ima Journal of Mathematical Control and Information,2006,23(2):127-136.
APA Zheng, J. H..(2006).Comparison of two linearization methods for optimal attitude maneuver of a non-linear flexible spacecraft.Ima Journal of Mathematical Control and Information,23(2),127-136.
MLA Zheng, J. H.."Comparison of two linearization methods for optimal attitude maneuver of a non-linear flexible spacecraft".Ima Journal of Mathematical Control and Information 23.2(2006):127-136.

入库方式: OAI收割

来源:国家空间科学中心

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