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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© 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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