Physics‐Based Approach to Thermospheric Density Estimation Using CubeSat GPS Data
Abstract In Low Earth Orbit (LEO), atmospheric drag is the largest contributor to trajectory prediction error. The current thermospheric density model used in operations, the High Accuracy Satellite Drag Model (HASDM), applies corrections to an empirical density model every 3 hr using observations o...
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Main Authors: | , , , |
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Format: | Article |
Language: | English |
Published: |
Wiley
2023-01-01
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Series: | Space Weather |
Subjects: | |
Online Access: | https://doi.org/10.1029/2021SW002997 |
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