A Novel Model for the Optimization of Interplanetary Trajectory Using Evolutionary Algorithm

Abstract

[1] T. R. Reppert, “Extending the patched-conic approximation to the restricted four-body problem,” AIAA Student Journal, Vol. 4, No. 1, pp.1–11, 2006.

[2] B.B.K. Reddy, B. Kimiaghalam, and A. Homaifar, “Evolutionary algorithms for parameter determination of patched conic approximation,” Aerospace Conference, 2005 IEEE, pp. 501-506, March 2005. doi: 10.1109/AERO.2005.1559340
http://dx.doi.org/10.1109/AERO.2005.1559340

[3] D. R. Myatt, V. M. Becerra, S. J. Nasuto, and J. M. Bishop, “Advanced global optimization tools for mission analysis and design,” Final Report of ESA Ariadna ITT AO4532/18138/04/NL/MV, Call03/4101, ESA, 2004.

[4] P. Di Lizia, G. Radice, “Advanced global optimization tools for mission analysis and design,” Final Report of ESA Ariadna ITT AO4532/18139/04/NL/MV,Call 03/4101, ESA, 2004.

[5] M. Vasile, “Design of Earth-Mars transfer trajectories using evolutionary-branching technique,” Acta Astronautica. pp. 705–720, 2005.
http://dx.doi.org/10.1016/j.actaastro.2004.12.002

[6] L. Casalino, M. R. Sentinella, “Evolutionary algorithm for interplanetary trajectories optimization,” New Trends in Astrodynamics and Applications V. 2008.

[7] B. Addis, A. Cassioli, M. Locatelli, and F. Schoen, “A global optimization method for the design of space trajectories,” Computational Optimization and Applications, 2009. doi: 10.1007/s10589-009-9261-6.
http://dx.doi.org/10.1007/s10589-009-9261-6

[8] M. Vasile, E. Minisci, and M. Locatelli, “On testing global optimization algorithms for space trajectory design,” AIAA/AAS Astrodynamics Specialist Conference and Exhibit, Honolulu, Hawaii, 2008.

[9] R. Storn, K. Price, “Differential evolution-a simple and efficient heuristic for global optimization over continuous spaces,” Journal of Global Optimization, Vol. 11, Dordrecht, pp. 341-359, 1997.

[10] R. Storn, “On the Usage of differential evolution for function optimization,” 1996 Biennial Conference of the North American Fuzzy Information Processing Society. pp. 519–523, 1996.

[11] Y. W. Leung, Y. Wang, “An orthogonal genetic algorithm with quantization for global numerical optimization,” IEEE Transactions on Evolutionary Computation, Vol. 5, NO. 1, pp. 41-53, 2001.
http://dx.doi.org/10.1109/4235.910464

[12] A. D. Olds, C. A. Kluever, and M. Cupples, “Interplanetary mission design using differential evolution,” Journal of Spacecraft and Rockets, Vol. 44, No. 5, pp. 1060–1070, 2007.
http://dx.doi.org/10.2514/1.27242

[13] A. B. Sergeyevsky, G. C. Snyder, and R. A. Cunniff, “Interplanetary mission design handbook, volume l, part 2: Earth to Mars Ballistic Mission Opportunities 1990-2005,” California: NASA JPL Publication 82-43, 1983.

[14] L. E. George, L. D. Kos, “Interplanetary Mission Design Handbook: Earth-to-Mars Mission Opportunities and Mars-to-Earth Return Opportunities 2009–2024,” NASA/TM—1998–208533, 1998.

[15] B. Addis, A. Cassioli, M. Locatelli, and F. Schoen, “Global optimization for the design of space trajectories,” published: Optimization OnLine, 2008.