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Mathematical Problems in Engineering
Volume 2012 (2012), Article ID 985429, 12 pages
http://dx.doi.org/10.1155/2012/985429
Research Article

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