Event-triggered adaptive attitude tracking control for spacecraft with unknown actuator faults

This paper is devoted to attitude tracking control of fractionated spacecraft with wireless communication. We consider the practical case that the spacecraft suffers from uncertain inertia parameters, external disturbances, and even unknown and time-varying actuator faults. Within the framework of t...

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Main Authors: Wang, Chenliang, Guo, Lei, Wen, Changyun, Hu, Qinglei, Qiao, Jianzhong
其他作者: School of Electrical and Electronic Engineering
格式: Article
語言:English
出版: 2022
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在線閱讀:https://hdl.handle.net/10356/155207
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