Satellite attitude control using three reaction wheels
This work addresses the attitude control of a satellite by applying MIMO quantitative feedback approach. The objective is to design a set of proper controllers in presence of unknown disturbances and parametric uncertainties for a nonlinear MIMO system. The physical model of satellite utilizes three...
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| Other Authors: | , , |
| Format: | article |
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2008
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| Online Access: | http://hdl.handle.net/10725/3960 http://dx.doi.org/10.1109/ACC.2008.4587262 http://libraries.lau.edu.lb/research/laur/terms-of-use/articles.php http://ieeexplore.ieee.org/xpls/abs_all.jsp?arnumber=4587262&tag=1 |
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