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Mathematical Problems in Engineering
Volume 2014, Article ID 820586, 8 pages
http://dx.doi.org/10.1155/2014/820586
Research Article

Satellite Attitude Control System Design Taking into Account the Fuel Slosh and Flexible Dynamics

1National Institute for Space Research (INPE), Avenida dos Astronautas 1758, 12227-010 São José dos Campos, SP, Brazil
2Brasília University, Campus Gama, Área Especial de Indústria-A-UnB, 72444-240 Brasilia, DF, Brazil

Received 31 March 2014; Revised 23 July 2014; Accepted 29 July 2014; Published 10 September 2014

Academic Editor: Antonio F. Bertachini A. Prado

Copyright © 2014 Alain G. de Souza and Luiz C. G. de Souza. 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

Alain G. de Souza and Luiz C. G. de Souza, “Satellite Attitude Control System Design Taking into Account the Fuel Slosh and Flexible Dynamics,” Mathematical Problems in Engineering, vol. 2014, Article ID 820586, 8 pages, 2014. https://doi.org/10.1155/2014/820586.