Robust Tracking Control Design for Spacecraft Under Control Input Saturation
A continuous globally stable tracking control algorithm is presented for spacecraft in the presence of control input saturation, parametric uncertainty, and external disturbances. The proposed control algorithm has the following properties: 1) fast and accurate response in the presence of bounded di...
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Veröffentlicht in: | Journal of guidance, control, and dynamics control, and dynamics, 2004-07, Vol.27 (4), p.627-633 |
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Format: | Artikel |
Sprache: | eng |
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