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International Journal of Aerospace Engineering
Volume 2016, Article ID 6346742, 11 pages
http://dx.doi.org/10.1155/2016/6346742
Research Article

A Multiconstrained Ascent Guidance Method for Solid Rocket-Powered Launch Vehicles

School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China

Received 28 March 2016; Accepted 28 June 2016

Academic Editor: Kenneth M. Sobel

Copyright © 2016 Si-Yuan Chen and Qun-Li Xia. 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

Si-Yuan Chen and Qun-Li Xia, “A Multiconstrained Ascent Guidance Method for Solid Rocket-Powered Launch Vehicles,” International Journal of Aerospace Engineering, vol. 2016, Article ID 6346742, 11 pages, 2016. https://doi.org/10.1155/2016/6346742.