A Novel Navigation Approach of Low Earth Orbit Satellites Formation Based on Reduced Relative Orbital Elements

Author:

Yang Shengqing,Du Yaoke,Wang Wenyan,Chen Junli,Wu Jingyu

Publisher

Springer Singapore

Reference28 articles.

1. Montenbruck, O., Gill, E.: Satellite Orbits-Models, Methods and Applications. Springer, Heidelberg, Germany (2000)

2. Montenbruck, O., Gill, E.: State interpolation for on-board navigation systems. Aerosp. Sci. Technol. 5(3), 209–220 (2001)

3. Wu, B.L., Cao, X.B., Ren, Z.W.: A long-time stable formation optimal design method for satellite formation. Acta Aeronautica et Astronaut Ica Sinica 28(1), 167–172 (2007). (Chinese)

4. Lin, L.X., Che, R.C.: Accurate dynamics models of satellite formation flying and 3-dimension positioning system. J. Astron. 29(3), 831–837 (2008). (Chinese)

5. Yin, J.F., Han, C.: Elliptical formation control based on relative orbit elements. Chin. J. Aeronaut. 26(6), 1554–1567 (2013)

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