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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Published in | Advances in space research Vol. 71; no. 9; pp. 3644 - 3660 |
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Main Authors | , , |
Format | Journal Article |
Language | English |
Published |
Elsevier B.V
01.05.2023
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Subjects | |
Online Access | Get full text |
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