Origin identification of sub-millimeter-sized debris from in-situ debris measurements
Origin identification of sub-millimeter-sized debris from in-situ debris measurements
This study introduces a new method to estimate the orbital parameters (inclination, nodal precession rate, and right ascension of the ascending node) of the broken-up object using in-situ debris measurements. To reduce collision probability with tiny debris generated from breakups of satellites, it is required to identify the origin of breakups and predict the orbit of debris. In general, small debris cannot be tracked from the ground, thus an in-situ measurement is an effective method to detect sub-millimeter-sized debris. Previous studies developed a method to identify the location of breakup origin from an in-situ measurement, however, it can be applied to an ideal situation where the detection occurs at the intersection of the orbit planes. This study introduces a new method to estimate the orbital parameters by fitting the model of geocentric declination to the measurement data. This method can be applied to practical situations that cannot be validated in previous studies. This paper also adopts iteratively reweighted least squares to improve estimation accuracy and mitigate initial value dependencies.
In-situ measurement, Orbit estimation, Orbit identification, Satellite fragmentation, Space debris
449-454
Tanahashi, Mahiro
84c2e4b3-5b94-4336-b4b5-97c7498d9273
Chen, Hongru
8286469d-afe1-46e5-b107-694017de4d97
Yoshimura, Yasuhiro
bee6a581-5176-46a6-8793-d539fa664489
Hanada, Toshiya
6a914261-4634-4e52-8605-7c7579869145
21 December 2023
Tanahashi, Mahiro
84c2e4b3-5b94-4336-b4b5-97c7498d9273
Chen, Hongru
8286469d-afe1-46e5-b107-694017de4d97
Yoshimura, Yasuhiro
bee6a581-5176-46a6-8793-d539fa664489
Hanada, Toshiya
6a914261-4634-4e52-8605-7c7579869145
Tanahashi, Mahiro, Chen, Hongru, Yoshimura, Yasuhiro and Hanada, Toshiya
(2023)
Origin identification of sub-millimeter-sized debris from in-situ debris measurements.
Acta Astronautica, 215, .
(doi:10.1016/j.actaastro.2023.12.038).
Abstract
This study introduces a new method to estimate the orbital parameters (inclination, nodal precession rate, and right ascension of the ascending node) of the broken-up object using in-situ debris measurements. To reduce collision probability with tiny debris generated from breakups of satellites, it is required to identify the origin of breakups and predict the orbit of debris. In general, small debris cannot be tracked from the ground, thus an in-situ measurement is an effective method to detect sub-millimeter-sized debris. Previous studies developed a method to identify the location of breakup origin from an in-situ measurement, however, it can be applied to an ideal situation where the detection occurs at the intersection of the orbit planes. This study introduces a new method to estimate the orbital parameters by fitting the model of geocentric declination to the measurement data. This method can be applied to practical situations that cannot be validated in previous studies. This paper also adopts iteratively reweighted least squares to improve estimation accuracy and mitigate initial value dependencies.
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More information
Accepted/In Press date: 17 December 2023
e-pub ahead of print date: 18 December 2023
Published date: 21 December 2023
Keywords:
In-situ measurement, Orbit estimation, Orbit identification, Satellite fragmentation, Space debris
Identifiers
Local EPrints ID: 490861
URI: http://eprints.soton.ac.uk/id/eprint/490861
ISSN: 0094-5765
PURE UUID: c03ff117-9419-46d6-9067-f333ce9a5b3a
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Date deposited: 07 Jun 2024 16:35
Last modified: 08 Jun 2024 02:12
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Contributors
Author:
Mahiro Tanahashi
Author:
Hongru Chen
Author:
Yasuhiro Yoshimura
Author:
Toshiya Hanada
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