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Mathematical Problems in Engineering
Volume 2012 (2012), Article ID 985429, 12 pages
doi:10.1155/2012/985429
Unscented Kalman Filter Applied to the Spacecraft Attitude Estimation with Euler Angles
1Space Mechanic and Control Division, INPE, 12227-010 São José dos Campos, SP, Brazil
2Department of Mathematics, FEG, UNESP, 12516-410 Guaratinguetá, SP, Brazil
Received 8 July 2011; Accepted 18 September 2011
Academic Editor: Antonio F. Bertachini A. Prado
Copyright © 2012 Roberta Veloso Garcia et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
How to Cite this Article
Roberta Veloso Garcia, Helio Koiti Kuga, and Maria Cecilia F. P. S. Zanardi, “Unscented Kalman Filter Applied to the Spacecraft Attitude Estimation with Euler Angles,” Mathematical Problems in Engineering, vol. 2012, Article ID 985429, 12 pages, 2012. doi:10.1155/2012/985429