Abstract
This paper takes research on the reason and elimination method of overall pseudo-rotation of navigation constellation. The inter-satellite ranging system errors can cause the overall pseudo-rotation of navigation constellation. In this paper, the reasons for overall pseudo-rotation of navigation constellation have been analyzed for four different systematic errors. Studies show that, short-cycle system errors and long-cycle system errors do not cause the overall pseudo-rotation, constant system errors may cause the overall pseudo-rotation, and linear system errors usually can cause the overall pseudo-rotation. When constant system errors or linear system errors of all satellites have the same direction, the overall pseudo-rotation of navigation constellation will occur. On this basis, this paper uses the overall pseudo-rotation correction algorithm to eliminate the overall pseudo-rotation of navigation constellation, simulation analysis shows that the algorithm can effectively eliminate the overall pseudo-rotation of navigation constellation. Finally, combining with the engineering practice of autonomous navigation, the paper gives the conclusions that on-board data processing units should adopt the overall pseudo-rotation correction algorithm to eliminate the overall pseudo-rotation of navigation constellation.
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References
Abusali, P. A. M., et al. (1998). Autonomous navigation of global positioning system satellites using crossing-link measurements. Journal of Guidance, Control, and Dynamics, 21(2), 321–327.
Rajan, J. A. (2002). Highlights of GPS II-R autonomous navigation. ION 58th Annual Meeting/CIGTF 21th Guidance Test Symposium, Albuquerque, NM, 24–26, June 2002.
Fisher, S. C., & Kamran, G. (1999). GPS IIF—The next generation. Proceeding of the IEEE, 87(1), 24–47.
Chen, J., Jiao, W., Ma, J. et al. (2005). Autonav of navigation satellite constellation based on crosslink range and orientation parameters constraining. Geomatics and Information Science of Wuhan University, 30(5), 439–443.
Wang, H., Chen, Z., Zheng, J., et al. (2011). A new algorithm for on-board autonomous orbit determination of navigation satellites. Journal of Navigation, 64, S162–S179.
Lin, L., & Yingchun, L. (2000). The deficient-rank problem of autonomous orbit determination based on satellite-to-satellite relative measurement. Journal of Spacecraft TT and C Technology, 19(3), 13–16.
Zhu, J., Liao, Y., & Wen, Y. (2009). The integrated autonomous orbit determination of the navigation constellation based on crosslink range and ground-based emitter. Journal of National University of Defense Technology, 31(2), 15–19.
Mean, M. D., & Bernstein, H. (1994). Ephemeris Observability Issues in the Global Positioning System Autonomous Navigation. IEEE Position Location and Navigation Symposium, New York, 677–680.
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© 2012 Springer-Verlag Berlin Heidelberg
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Wang, H., Han, X., He, S., Chu, H., Wu, X. (2012). The Correction Method of Overall Pseudo-Rotation on Autonomous Navigation of Navigation Constellation. In: Sun, J., Liu, J., Yang, Y., Fan, S. (eds) China Satellite Navigation Conference (CSNC) 2012 Proceedings. Lecture Notes in Electrical Engineering, vol 160. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-29175-3_26
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DOI: https://doi.org/10.1007/978-3-642-29175-3_26
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