Adaptive Neural Network Control of a Flexible Spacecraft Subject to Input Nonlinearity and Asymmetric Output Constraint

This article focuses on the vibration reducing and angle tracking problems of a flexible unmanned spacecraft system subject to input nonlinearity, asymmetric output constraint, and system parameter uncertainties. Using the backstepping technique, a boundary control scheme is designed to suppress the...

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Bibliographic Details
Published inIEEE Transactions on Neural Networks and Learning Systems Vol. 33; no. 11; pp. 6226 - 6234
Main Authors Liu, Yu, Chen, Xiongbin, Wu, Yilin, Cai, He, Yokoi, Hiroshi
Format Journal Article
LanguageEnglish
Published United States IEEE 01.11.2022
Institute of Electrical and Electronics Engineers (IEEE)
The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
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