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

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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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  Data: <searchLink fieldCode="JN" term="%22Asian+Journal+of+Control%22">Asian Journal of Control</searchLink>; Mar2021, Vol. 23 Issue 2, p1003-1024, 22p
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      – Type: doi
        Value: 10.1002/asjc.2277
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      – Code: eng
        Text: English
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        PageCount: 22
        StartPage: 1003
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      – TitleFull: Finite‐time adaptive fault‐tolerant control for rigid spacecraft attitude tracking.
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            NameFull: Gao, Shihong
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            NameFull: Jing, Yuanwei
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            NameFull: Liu, Xiaoping
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              Text: Mar2021
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              Y: 2021
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              Value: 23
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