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• W4313444524 endingPage "110814" @default.
• W4313444524 startingPage "110814" @default.
• W4313444524 abstract "As one of attitude representation methods for a rigid body, the rotation matrices defined on the special orthogonal matrix group SO(3) can give the unique, global and nonsingular solution. For the attitude control systems evolving on Lie group SO(3)×R3, a second-order sliding surface is constructed and proved to be a Lie subgroup, along which the reduced-order dynamics is almost globally asymptotically stable at the equilibrium state. Based on the new sliding-mode surface, a fault-tolerant controller is designed to deal with the actuator faults and external disturbances in attitude control systems. The new method is numerically simulated and further implemented in a semi-physical simulation system of an air-bearing platform to verify its effectiveness in spacecraft practical engineering." @default.
• W4313444524 created "2023-01-06" @default.
• W4313444524 creator A5004841687 @default.
• W4313444524 creator A5071047366 @default.
• W4313444524 creator A5081517523 @default.
• W4313444524 date "2023-03-01" @default.
• W4313444524 modified "2023-10-16" @default.
• W4313444524 title "Second-order sliding-mode on SO(3) and fault-tolerant spacecraft attitude control" @default.
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• W4313444524 doi "https://doi.org/10.1016/j.automatica.2022.110814" @default.
• W4313444524 hasPublicationYear "2023" @default.
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