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International Journal of Aerospace Engineering
Volume 2017 (2017), Article ID 9234905, 10 pages
https://doi.org/10.1155/2017/9234905
Research Article

A Shape-Based Method for Continuous Low-Thrust Trajectory Design between Circular Coplanar Orbits

1National Key Laboratory of Aerospace Flight Dynamics, Xi’an, Shaanxi 710072, China
2School of Astronautics, Northwestern Polytechnical University, Xi’an, Shaanxi 710072, China

Correspondence should be addressed to Qun Fang; nc.ude.upwn@gnafq

Received 16 December 2016; Accepted 22 March 2017; Published 10 April 2017

Academic Editor: Paul Williams

Copyright © 2017 Qun Fang 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.

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