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Study of the Two-Line Element Accuracy by 1U CubeSat with a GPS Receiver
There is a common practice to calculate orbital trajectories of space objects like satellites and space debris using Two-Line Element Sets (TLEs). However, TLEs provide rather coarse parameters for fine orbit computation and their precision varies with age of their issue and position of the satellit...
| Autores principales: | , , |
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| Formato: | Online Artículo Texto |
| Lenguaje: | English |
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MDPI
2022
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| Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9030488/ https://www.ncbi.nlm.nih.gov/pubmed/35458886 http://dx.doi.org/10.3390/s22082902 |