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
Hauptverfasser: Boskovic, Jovan D, Li, Sai-Ming, Mehra, Raman K
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Sprache:eng
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