Finite-Time Attitude Tracking Control for Spacecraft Using Terminal Sliding Mode and Chebyshev Neural Network

标题
Finite-Time Attitude Tracking Control for Spacecraft Using Terminal Sliding Mode and Chebyshev Neural Network
作者
关键词
-
出版商
Institute of Electrical and Electronics Engineers (IEEE)
发表日期
2011-01-25
DOI
10.1109/tsmcb.2010.2101592

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