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Mathematical Problems in Engineering
Volume 2006 (2006), Article ID 34317, 20 pages
http://dx.doi.org/10.1155/MPE/2006/34317

Alternative paths to Earth-Moon transfer

1Programa de Pós-graduação em Engenharia e Tecnologia Espaciais, Instituto Nacional de Pesquisas Espaciais (INPE), São José dos Campos, SP 12245-970, Brazil
2Grupo de Dinâmica Orbital & Planetologia, Universidade Estadual Paulista (UNESP), Campus Guaratinguetá, Guaratinguetá, SP 12516-410, Brazil

Received 28 December 2004; Revised 27 July 2005; Accepted 23 August 2005

Copyright © 2006 Cristiano Fiorilo de Melo and Othon Cabo Winter. 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. R. R. Bate, D. D. Mueller, and J. E. White, Fundamentals of Astrodynamics, Dover, New York, 1971.
  2. E. A. Belbruno, “Lunar capture orbits, a method of constructing earth moon trajectories and the lunar gas mission,” in Proceedings of 19th AIAA/DGLR/JSASS International Electric Propulsion Conference, Colorado Springs, Colorado, 1987, AIAA-87-1054.
  3. E. A. Belbruno, “Examples of the nonlinear dynamics of ballistic capture an escape in earth moon system,” in Proceedings of AIAA Astrodynamics Conference (Oregon, 1990), pp. 179–184, American Institute of Aeronautics and Astronautics, Washington, DC, 1990, AIAA-90-2896.
  4. E. A. Belbruno, “Ballistic lunar capture transfer using the fuzzy boundary and solar perturbations: a survey,” in Proceedings of International Congress of SETI Sail and Astrodynamics (Turin, 1992), 1992.
  5. E. A. Belbruno, “Through the fuzzy boundary: a new route the moon,” The Planetary Report, vol. 7, no. 3, pp. 8–10, 1992. View at Google Scholar
  6. E. A. Belbruno and J. K. Miller, “A ballistic lunar capture trajectory for Japanese spacecraft Hiten,” International Document JPL IOM 312/90.4-1731, Jet Propulsion Laboratory, California Institute of Technology, California, 1990. View at Google Scholar
  7. E. A. Belbruno and J. K. Miller, “Ballistic lunar capture for the lunar observe,” Internal Document IOM 212/90.4-1752, Jet propulsion Laboratory, California Institute of Technology, California, 1990. View at Google Scholar
  8. R. A. Broucke, “Periodic orbits in the restricted three-body problem with earth-moon masses,” Tech. Rep. 32-1168, Jet Propulsion Laboratory, California Institute of Technology, California, 1968. View at Google Scholar
  9. A. Brunini, “On the satellite capture problem, capture and stability regions for planetary satellites,” Celestial Mechanics & Dynamical Astronomy., vol. 64, no. 1-2, pp. 79–92, 1996. View at Google Scholar · View at Zentralblatt MATH
  10. W. C. Feldman, B. L. Barraclough, S. Maurice et al., “Major compositional units of the moon: lunar prospector thermal and fast neutrons,” Science, vol. 281, no. 5382, pp. 1489–1493, 1998. View at Google Scholar
  11. W. S. Koon, M. W. Lo, J. E. Marsden, and S. D. Ross, “Low energy transfer to the moon,” Celestial Mechanics & Dynamical Astronomy., vol. 81, no. 1-2, pp. 63–73, 2001. View at Publisher · View at Google Scholar · View at Zentralblatt MATH · View at MathSciNet
  12. V. Krish, E. A. Belbruno, and W. M. Hollister, “An investigation into critical aspects of a new form of low energy lunar transfer, the Belbruno-Miller trajectories,” in AIAA/AAS Astrodynamics Conference (South Carolina, 1990), pp. 435–444, American Institute of Aeronautics and Astronautics, Washington, DC, 1992, AIAA-1992-4581.
  13. M. W. Lo and S. D. Ross, “Low energy interplanetary transfers using invariant manifolds of L1, L2 and halo orbits,” in Proceedings of AAS/AIAA Space Flight Mechanics Meeting (California, 1998), 1998.
  14. J. K. Miller and E. A. Belbruno, “A method for construction of a lunar transfer trajectories using ballistic capture,” in Proceedings of 1st AAS/AIAA Annual Spaceflight Mechanics Meeting (Texas, 1991), pp. 97–109, 1991, AAS-91-1000.
  15. M. A. Murison, “The fractal dynamics of satellite capture in the circular restricted three-body problem,” Astronom. J., vol. 98, no. 6, pp. 2346–2359, 1989. View at Google Scholar
  16. C. D. Murray and S. F. Dermott, Solar System Dynamics, Cambridge University Press, Cambridge, 1999. View at Zentralblatt MATH · View at MathSciNet
  17. C. A. Ocampo, “Transfers to earth centered orbits via lunar gravity assist,” Acta Astronaut., vol. 52, no. 2, pp. 173–179, 2003. View at Google Scholar
  18. A. F. B. A. Prado, “Minimun fuel trajectories for the lunar polar orbiter,” Revista Brasileira de Automação e Controle (SBA)., vol. 12, no. 2, pp. 163–170, 2001 (Portuguese). View at Google Scholar
  19. A. F. B. A. Prado, “A numerical study of the gravitational capture in the bi-circular restricted four-body problem,” in Proceedings of 54th International Astronautical Congress (Bremen, 2003), 2003, IAC-03-A.1.01.
  20. A. F. B. A. Prado and E. Vieira Neto, “Orbital maneuvers using gravitational capture, nonlinear dynamics, chaos, control and their applications to engineering sciences,” in New Trends in Dynamics and Control, J. M. Baltazar, P. B. Gonçalves, and R. M. F. L. R. F. Brazil, Eds., vol. 3, pp. 109–128, 2002. View at Google Scholar
  21. P. A. Regeon, P. R. Lynn, M. Johnson, and R. J. Chapman, “The clementine lunar orbiter,” in Proceedings of 20th GIFU ISTS & 11th IAS, Paper no. 96-e-40, 2002.
  22. O. C. Winter, E. Vieira Neto, and A. F. B. A. Prado, “Orbital maneuvers using gravitational capture times,” Advances in Space Research, vol. 31, no. 8, pp. 2005–2010, 2003. View at Google Scholar
  23. H. Yamakawa, On earth-moon transfer trajectory with gravitational capture, Ph.D. dissertation, University of Tokyo, Tokyo, 1992.