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Finite‐time adaptive fault‐tolerant control for rigid spacecraft attitude tracking.

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Bibliographic Details
Title: Finite‐time adaptive fault‐tolerant control for rigid spacecraft attitude tracking.
Authors: Gao, Shihong1,2, Jing, Yuanwei1, ywjjing@mail.neu.edu.cn, Liu, Xiaoping3, Dimirovski, Georgi M.4
Source: Asian Journal of Control; Mar2021, Vol. 23 Issue 2, p1003-1024, 22p
Database: Applied Science & Technology Source
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Description
ISSN:15618625
DOI:10.1002/asjc.2277