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Mathematical Problems in Engineering
Volume 2009, Article ID 242396, 18 pages
http://dx.doi.org/10.1155/2009/242396
Research Article

Spin-Stabilized Spacecrafts: Analytical Attitude Propagation Using Magnetic Torques

1Space Mechanic and Control Division, National Institute for Space Research (INPE), Sao Paulo, São José dos Campos 12227-010, Brazil
2Department of Mathematics, Group of Orbital Dynamics and Planetology, Sao Paulo State University (UNESP), Sao Paulo, Guaratinguetá 12516-410, Brazil

Received 28 July 2009; Accepted 4 November 2009

Academic Editor: Antonio Prado

Copyright © 2009 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, Maria Cecília F. P. S. Zanardi, and Hélio Koiti Kuga, “Spin-Stabilized Spacecrafts: Analytical Attitude Propagation Using Magnetic Torques,” Mathematical Problems in Engineering, vol. 2009, Article ID 242396, 18 pages, 2009. https://doi.org/10.1155/2009/242396.