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Mathematical Problems in Engineering
Volume 2014, Article ID 359845, 15 pages
http://dx.doi.org/10.1155/2014/359845
Research Article

Effects of the Eccentricity of a Perturbing Third Body on the Orbital Correction Maneuvers of a Spacecraft

1Universidade Estadual Paulista (UNESP), São João da Boa Vista, SP, Brazil
2Instituto Nacional de Pesquisas Espaciais (INPE), 12227-010 São José dos Campos, SP, Brazil
3Universidade Estadual Paulista (UNESP), 12516-410 Guaratinguetá, SP, Brazil

Received 25 January 2014; Revised 21 April 2014; Accepted 17 May 2014; Published 3 July 2014

Academic Editor: Maria Cecilia Zanardi

Copyright © 2014 R. C. Domingos 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

R. C. Domingos, A. F. B. A. Prado, and V. M. Gomes, “Effects of the Eccentricity of a Perturbing Third Body on the Orbital Correction Maneuvers of a Spacecraft,” Mathematical Problems in Engineering, vol. 2014, Article ID 359845, 15 pages, 2014. https://doi.org/10.1155/2014/359845.