Article ID Journal Published Year Pages File Type
1764304 Advances in Space Research 2015 13 Pages PDF
Abstract
The results show that the reduction in accuracy is not extensive and good orbit predictions are still possible when using only 5 s of data from the beginning of each pass. The results are achievable due to an accurate ballistic coefficient estimation and accurate tracking data. The dependence of the results on the perigee altitude of the objects is obvious, indicating modelling error of the atmospheric mass density in lower orbits remains the dominant source of error.
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Related Topics
Physical Sciences and Engineering Earth and Planetary Sciences Space and Planetary Science
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