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Mathematical Problems in Engineering
Volume 2007, Article ID 98532, 9 pages
http://dx.doi.org/10.1155/2007/98532
Research Article

Orbital Maneuvers Using Low Thrust to Place a Satellite in a Constellation

Division of Space Dynamics and Control, Instituto Nacional de Pesquisas Espaciais (INPE), Avenue dos Astronautas, 1758 Jardim da Granja, São José dos Campos, SP 12227-010, Brazil

Received 19 April 2006; Revised 20 September 2006; Accepted 19 October 2006

Academic Editor: José Manoel Balthazar

Copyright © 2007 Vivian Martins Gomes 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.

Linked References

  1. D. J. Stewart and R. G. Melton, “Approximate analytic representations for low-thrust trajectories,” Advances in the Astronautical Sciences, vol. 76, no. 2, pp. 1455–1467, 1991. View at Google Scholar
  2. S. Geffroy and R. Epenoy, “Optimal low-thrust transfers with constraints—generalization of averaging techniques,” Acta Astronautica, vol. 41, no. 3, pp. 133–149, 1997. View at Publisher · View at Google Scholar
  3. C. A. Kluever and S. R. Oleson, “A direct approach for computing near optimal low-thrust transfers,” Advances in the Astronautical Sciences, vol. 97, no. 2, pp. 1783–1800, 1997. View at Google Scholar
  4. J. A. Kechichian, “Optimal low-earth-orbit-geostationary-earth-orbit intermediate acceleration orbit transfer,” Journal of Guidance, Control and Dynamics, vol. 20, no. 4, pp. 803–811, 1997. View at Google Scholar
  5. A. L. Herman and D. B. Spencer, “Optimal, low-thrust earth orbit transfers using higher-order collocation methods,” Journal of Guidance, Control and Dynamics, vol. 25, no. 1, pp. 40–47, 2002. View at Google Scholar
  6. B. M. Kiforenko, Z. V. Pasechnik, S. B. Kyrychenko, and I. Y. Vasiliev, “Minimum time transfers of a low-thrust rocket in strong gravity fields,” Acta Astronautica, vol. 52, no. 8, pp. 601–611, 2003. View at Publisher · View at Google Scholar
  7. T. Haberkorn, P. Martinon, and J. Gergaud, “Low-thrust minimum-fuel orbital transfer: a homotopic approach,” Journal of Guidance, Control and Dynamics, vol. 27, no. 6, pp. 1046–1059, 2004. View at Google Scholar
  8. A. F. B. A. Prado, Análise, Seleção e Implementação de Procedimentos que Visem Manobras Ótimas em Órbitas de Satélites Artificiais, Master Thesis, INPE, São José dos Campos, Brazil, 1989.
  9. A. F. B. A. Prado and A. Rios-Neto, “Um estudo bibliográfico sobre o problema de transferências de órbitas,” Revista Brasileira de Ciências Mecânicas, vol. 15, no. 1, pp. 65–78, 1993. View at Google Scholar
  10. M. C. B. Biggs, The Optimisation of Spacecraft Orbital Manoeuvres. Part I: Linearly Varying Thrust Angles, The Hattfield Polytechnic Numerical Optimisation Centre, Hartford, Conn, USA, 1978.
  11. W. H. Press, B. P. Flannery, S. A. Teukolsky, and W. T. Vetterling, Numerical Recipes, Cambridge University Press, NewYork, NY, USA, 1989.