中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Finite-Time Attitude Tracking Control for Spacecraft Using Terminal Sliding Model and Chebyshev Neural Network (vol 41, pg 950, 2011)

文献类型:期刊论文

作者Zou, An-Min1; Kumar, Krishna Dev1; Hou, Zeng-Guang2
刊名IEEE TRANSACTIONS ON CYBERNETICS
出版日期2013-04-01
卷号43期号:2页码:803-803
WOS标题词Science & Technology ; Technology
类目[WOS]Computer Science, Artificial Intelligence ; Computer Science, Cybernetics
研究领域[WOS]Computer Science
收录类别SCI
语种英语
WOS记录号WOS:000317644300032
源URL[http://ir.ia.ac.cn/handle/173211/3476]  
专题自动化研究所_复杂系统管理与控制国家重点实验室_先进机器人控制团队
作者单位1.Ryerson Univ, Dept Aerosp Engn, Toronto, ON M5B 2K3, Canada
2.Chinese Acad Sci, Inst Automat, Key Lab Complex Syst & Intelligence Sci, Beijing 100190, Peoples R China
推荐引用方式
GB/T 7714
Zou, An-Min,Kumar, Krishna Dev,Hou, Zeng-Guang. Finite-Time Attitude Tracking Control for Spacecraft Using Terminal Sliding Model and Chebyshev Neural Network (vol 41, pg 950, 2011)[J]. IEEE TRANSACTIONS ON CYBERNETICS,2013,43(2):803-803.
APA Zou, An-Min,Kumar, Krishna Dev,&Hou, Zeng-Guang.(2013).Finite-Time Attitude Tracking Control for Spacecraft Using Terminal Sliding Model and Chebyshev Neural Network (vol 41, pg 950, 2011).IEEE TRANSACTIONS ON CYBERNETICS,43(2),803-803.
MLA Zou, An-Min,et al."Finite-Time Attitude Tracking Control for Spacecraft Using Terminal Sliding Model and Chebyshev Neural Network (vol 41, pg 950, 2011)".IEEE TRANSACTIONS ON CYBERNETICS 43.2(2013):803-803.

入库方式: OAI收割

来源:自动化研究所

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