An improved method for LEO orbit prediction using predicted accelerometer data
Author:
Funder
Key Research and Development Program of Hubei Province
National Natural Science Foundation of China
Publisher
Springer Science and Business Media LLC
Link
https://link.springer.com/content/pdf/10.1007/s10291-024-01676-w.pdf
Reference37 articles.
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2. Avanzini G, de Angelis EL, Giulietti F, Serrano N (2019) Attitude control of low earth orbit satellites by reaction wheels and magnetic torquers. Acta Astronaut 160:625–634. https://doi.org/10.1016/j.actaastro.2019.03.013
3. Berger C, Biancale R, Barlier F (1998) Improvement of the empirical thermospheric model DTM: DTM94–a comparative review of various temporal variations and prospects in space geodesy applications. J Geod 72:161–178. https://doi.org/10.1007/s001900050158
4. Ge H, Li B, Ge M, Zang N, Nie L, Shen Y, Schuh H (2018) Initial assessment of precise point positioning with LEO enhanced global navigation satellite systems (LeGNSS). Remote Sens 10(7):984. https://doi.org/10.3390/rs10070984
5. Ge H, Li B, Ge M, Nie L, Schuh H (2020a) Improving low earth orbit (LEO) prediction with accelerometer data. Remote Sens 12(10):1599. https://doi.org/10.3390/rs12101599
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