Revisiting filtering of two-line element sets for higher precision ephemerides
File(s)issfd2024_paper_submitted.pdf (2.89 MB)
Accepted version
Author(s)
Hallgarten La Casta, Max
Amato, Davide
Type
Conference Paper
Abstract
The availability of accurate and timely state
predictions for objects in near-Earth orbits is becoming
increasingly important due to the growing congestion in
key orbital regimes. The Two-line Element Set (TLE)
catalogue remains, to this day, one of the few publicly-
available, comprehensive sources of near-Earth object
ephemerides. At the same time, TLEs are limited by their
corresponding low-fidelity physical models, introducing
errors and uncertainty into state predictions. Previous
literature has shown that filtering TLEs with batch least
squares methods can yield significant improvements in
long-term state prediction accuracy. However, this pro-
cess can be highly sensitive to TLE quality which can
vary throughout the year. It will be shown that remov-
ing systematic biases in along-track position prior to state
estimation can reduce post-fit position errors by an order
of magnitude for selected satellites in the Medium Earth
Orbit (MEO) regime.
predictions for objects in near-Earth orbits is becoming
increasingly important due to the growing congestion in
key orbital regimes. The Two-line Element Set (TLE)
catalogue remains, to this day, one of the few publicly-
available, comprehensive sources of near-Earth object
ephemerides. At the same time, TLEs are limited by their
corresponding low-fidelity physical models, introducing
errors and uncertainty into state predictions. Previous
literature has shown that filtering TLEs with batch least
squares methods can yield significant improvements in
long-term state prediction accuracy. However, this pro-
cess can be highly sensitive to TLE quality which can
vary throughout the year. It will be shown that remov-
ing systematic biases in along-track position prior to state
estimation can reduce post-fit position errors by an order
of magnitude for selected satellites in the Medium Earth
Orbit (MEO) regime.
Date Issued
2024-04-22
Date Acceptance
2024-01-30
Citation
2024
Copyright Statement
© 2024 The Author(s). This is the author’s accepted manuscript made available under a CC-BY licence in accordance with Imperial’s Research Publications Open Access policy (www.imperial.ac.uk/oa-policy)
License URL
Source
29th International Symposium on Spaceflight Dynamics (ISSFD)
Publication Status
Published
Start Date
2024-04-22
Finish Date
2024-04-26
Coverage Spatial
European Space Operations Centre (ESOC), Darmstadt, Germany