Robust dynamic surface sliding mode control for attitude tracking of flexible spacecraft with an extended state observer
The nonlinear attitude motion equations of flexible spacecraft described by the Euler angles are expressed in the vector form. Based on dynamic surface control, a new robust dynamic surface sliding mode controller is proposed for the attitude tracking and active vibration suppression of flexible spa...
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Veröffentlicht in: | Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering Journal of aerospace engineering, 2017-03, Vol.231 (3), p.533-547 |
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Format: | Artikel |
Sprache: | eng |
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