Finite-time active fault-tolerant attitude control for flexible spacecraft with vibration suppression and anti-unwinding

In this paper, a finite-time active fault-tolerant control scheme is designed for a flexible spacecraft’s attitude control experiencing inertial parametric variations, external disturbances, multiple actuator faults, and estimation errors while suppressing the flexible appendages’ vibrations without...

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Bibliographic Details
Published inAdvances in space research Vol. 71; no. 9; pp. 3644 - 3660
Main Authors Hasan, Muhammad Noman, Haris, Muhammad, Qin, Shiyin
Format Journal Article
LanguageEnglish
Published Elsevier B.V 01.05.2023
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