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Mathematical Problems in Engineering
Volume 2014, Article ID 602724, 7 pages
http://dx.doi.org/10.1155/2014/602724
Research Article

Relative Status Determination for Spacecraft Relative Motion Based on Dual Quaternion

1Research Center of Satellite Technology, Harbin Institute of Technology, Harbin 150080, China
2Shanghai Institute of Space Flight Control Technology, Shanghai 200030, China
3College of Aerospace and Civil Engineering, Harbin Engineering University, Harbin 150001, China

Received 26 February 2014; Accepted 7 April 2014; Published 8 May 2014

Academic Editor: Weichao Sun

Copyright © 2014 Jun Sun 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

Jun Sun, Shijie Zhang, Xiande Wu, Fengzhi Guo, and Yaen Xie, “Relative Status Determination for Spacecraft Relative Motion Based on Dual Quaternion,” Mathematical Problems in Engineering, vol. 2014, Article ID 602724, 7 pages, 2014. https://doi.org/10.1155/2014/602724.