Accuracy Assessment of Geostationary-Earth-Orbit with Simplified Perturbations Models
By: Lihua Ma, Xiaojun Xu and Feng Pang
References
- Kelso, T. (1998) Frequently asked questions: two-line element set format., Vol. 4, No. 3, 52-54
- Ma L., Hu C., and Pei J. (2016) A novel polarization tracking method for Earth station antenna., Vol. 5, No. 1, 10-19
- Ma L., Jing Y., Ji H, and Zhang L. (2011) Analysis of evolution of orbits of GEO satellites near end of life based on the STK software. Astronomical Research & Technology, Vol. 8, No. 4, 347-353
- Roddy D. (2006). McGraw-Hill.
- Vallado D., Crawford P, Hujsak R, and Kelso T. (2006) Revisiting spacetrack report # 3., 2006-6753
- Wei D, and Zhao C. (2009) Analysis on the accuracy of the SGP4/SDP4 model., Vol. 50, No. 3, 333-339
- Yang Y. (2005). Beijing: National Defense Industry Press.
DOI: https://doi.org/10.1515/arsa-2016-0005 | Journal eISSN: 2083-6104 | Journal ISSN: 1509-3859 (formerly 0208-841X)
Language: English
Page range: 55 - 59
Submitted on: Oct 8, 2015
Accepted on: Mar 4, 2016
Published on: May 28, 2016
Published by: Polish Academy of Sciences, Space Research Centre
In partnership with: Paradigm Publishing Services
Related subjects:
© 2016 Lihua Ma, Xiaojun Xu, Feng Pang, published by Polish Academy of Sciences, Space Research Centre
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.