Nonlinear attitude and shape control of spacecraft with articulated appendages and reaction wheels
Three-dimensional attitude and shape control problems are studied for a class of spacecraft with articulated appendages and reaction wheels. A number of special cases of such attitude control problems have been studied previously. We provide a unified formulation and a comprehensive set of results f...
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Veröffentlicht in: | IEEE transactions on automatic control 2000-08, Vol.45 (8), p.1455-1469 |
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Sprache: | eng |
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