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International Journal of Aerospace Engineering
Volume 2012 (2012), Article ID 910496, 13 pages
http://dx.doi.org/10.1155/2012/910496
Research Article

Implementation of a Differential Geometric Filter for Spacecraft Formation Orbit Estimation

1MEEM Department, Michigan Technological University, Houghton, MI 49931, USA
2ECE Department, Michigan Technological University, Houghton, MI 49931, USA

Received 31 May 2011; Revised 31 August 2011; Accepted 11 October 2011

Academic Editor: Srinivas R. Vadali

Copyright © 2012 Shu Ting Goh 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

Shu Ting Goh, Ossama Abdelkhalik, and Seyed A. (Reza) Zekavat, “Implementation of a Differential Geometric Filter for Spacecraft Formation Orbit Estimation,” International Journal of Aerospace Engineering, vol. 2012, Article ID 910496, 13 pages, 2012. doi:10.1155/2012/910496