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International Journal of Aerospace Engineering
Volume 2015, Article ID 723414, 11 pages
Research Article

GPS Based Reduced-Dynamic Orbit Determination for Low Earth Orbiters with Ambiguity Fixing

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

Received 29 March 2015; Accepted 31 May 2015

Academic Editor: Paolo Tortora

Copyright © 2015 Yang Yang 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.

Citations to this Article [1 citation]

The following is the list of published articles that have cited the current article.

  • Yang Xiao, Limin Li, Jiachao Chang, Kang Wu, Guang Liang, and Jinpei Yu, “A Novel GPS Based Real Time Orbit Determination Using Adaptive Extended Kalman Filter,” IEICE Transactions on Fundamentals of Electronics, Communications and Computer Sciences, vol. E101.A, no. 1, pp. 287–292, 2018. View at Publisher · View at Google Scholar