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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Bibliographic Details
Main Authors: Wang, Chenliang, Guo, Lei, Wen, Changyun, Hu, Qinglei, Qiao, Jianzhong
Other Authors: School of Electrical and Electronic Engineering
Format: Article
Language:English
Published: 2022
Subjects:
Online Access:https://hdl.handle.net/10356/155207
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Institution: Nanyang Technological University
Language: English