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Mathematical Problems in Engineering
Volume 2015, Article ID 949480, 13 pages
http://dx.doi.org/10.1155/2015/949480
Research Article

Spacecraft Multiple-Impulse Trajectory Optimization Using Differential Evolution Algorithm with Combined Mutation Strategies and Boundary-Handling Schemes

College of Aerospace Science and Engineering, National University of Defense Technology, Changsha, Hunan 410073, China

Received 25 January 2015; Revised 7 April 2015; Accepted 14 April 2015

Academic Editor: Yakov Strelniker

Copyright © 2015 Yuehe Zhu 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

Yuehe Zhu, Hua Wang, and Jin Zhang, “Spacecraft Multiple-Impulse Trajectory Optimization Using Differential Evolution Algorithm with Combined Mutation Strategies and Boundary-Handling Schemes,” Mathematical Problems in Engineering, vol. 2015, Article ID 949480, 13 pages, 2015. https://doi.org/10.1155/2015/949480.