Abstract
The problem of determining the trajectory parameters of a small satellite using a satellite navigation equipment is studied. A raw data processing algorithm is proposed when the measurements from a global navigation satellite system are not always regular.
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References
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Original Russian Text © A.A. Golovan, A. Cepe, 2016, published in Vestnik Moskovskogo Universiteta, Matematika. Mekhanika, 2016, Vol. 71, No. 1, pp. 64–68.
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Golovan, A.A., Cepe, A. Determination of trajectory parameters for a small satellite using raw satellite measurements. Moscow Univ. Mech. Bull. 71, 19–22 (2016). https://doi.org/10.3103/S0027133016010040
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DOI: https://doi.org/10.3103/S0027133016010040