Polarimetric tomography applied to synthetic multi-spacecraft white-light images: observing coronal mass ejections in 3D

ABSTRACT A discrete tomography method has been developed that is able to reconstruct 3D coronal mass ejection (CME) density structure. We test the method by producing synthetic coronagraph imagery for three events using the CORona–HELiosphere (CORHEL) model. We combine images from different numbers of observing spacecraft and we perform the method separately using polarimetric and non-polarimetric reconstructions, as a means to test their relative effectiveness. We show that increasing the number of observing spacecraft consistently reduces the mean relative absolute error (MRAE) between the simulated and reconstructed density. Furthermore, the MRAE is generally lower when using polarimetric reconstructions compared to non-polarimetric reconstructions. Methods applied to localize the CME front work well for all spacecraft configurations, and are improved when using polarimetric, over non-polarimetric, reconstructions. The presence of a CME front can be identified with an accuracy of $(72\pm 9)\, \rm per\,cent$, $(70\pm 8)\, \rm per\,cent$, and $(52\pm 12)\, \rm per\,cent$ for CME1, CME2, and CME3 via polarimetric reconstructions using only three spacecraft at L1, L4, and L5. The radial position of the CME front can be constrained to a high level of precision when using polarimetric reconstructions using the same three spacecraft; $0.003\pm 0.004$ , $0.004\pm 0.005$ , and $0.005\pm 0.004$ au for CME1, CME2, and CME3, respectively. We expect that at least four spacecraft are required in order to derive accurate information about 3D CME structure. We find no strong evidence of improvement when including out-of-ecliptic observers, but that their inclusion increases the volume of space within which the inversion can be performed.

Authors

Institutions

Publication Details

Journal
Monthly Notices of the Royal Astronomical Society
Published
2026-04-30
DOI
https://doi.org/10.1093/mnras/stag818
Primary Topic
Solar and Space Plasma Dynamics
Type
article
Field-Weighted Citation Impact
0.00

Funders

Controls
|||
ALL TIME
JAN
FEB
MAR
APR
MAY
JUN
JUL
AUG
SEP
OCT
article

Polarimetric tomography applied to synthetic multi-spacecraft white-light images: observing coronal mass ejections in 3D

Greta M. Cappello, Eleanna Asvestari, Jaša Čalogović, Maike Bauer et al.
Monthly Notices of the Royal Astronomical Society
Solar and Space Plasma Dynamics
article

Polarimetric tomography applied to synthetic multi-spacecraft white-light images: observing coronal mass ejections in 3D

Greta M. Cappello, Eleanna Asvestari, Jaša Čalogović, Maike Bauer, Luke Barnard, David Barnes, Christina Kay, Phillip Hess, Tanja Amerstorfer, Erika Palmerio
article en

Abstract

ABSTRACT A discrete tomography method has been developed that is able to reconstruct 3D coronal mass ejection (CME) density structure. We test the method by producing synthetic coronagraph imagery for three events using the CORona–HELiosphere (CORHEL) model. We combine images from different numbers of observing spacecraft and we perform the method separately using polarimetric and non-polarimetric reconstructions, as a means to test their relative effectiveness. We show that increasing the number of observing spacecraft consistently reduces the mean relative absolute error (MRAE) between the simulated and reconstructed density. Furthermore, the MRAE is generally lower when using polarimetric reconstructions compared to non-polarimetric reconstructions. Methods applied to localize the CME front work well for all spacecraft configurations, and are improved when using polarimetric, over non-polarimetric, reconstructions. The presence of a CME front can be identified with an accuracy of $(72\pm 9)\, \rm per\,cent$, $(70\pm 8)\, \rm per\,cent$, and $(52\pm 12)\, \rm per\,cent$ for CME1, CME2, and CME3 via polarimetric reconstructions using only three spacecraft at L1, L4, and L5. The radial position of the CME front can be constrained to a high level of precision when using polarimetric reconstructions using the same three spacecraft; $0.003\pm 0.004$ , $0.004\pm 0.005$ , and $0.005\pm 0.004$ au for CME1, CME2, and CME3, respectively. We expect that at least four spacecraft are required in order to derive accurate information about 3D CME structure. We find no strong evidence of improvement when including out-of-ecliptic observers, but that their inclusion increases the volume of space within which the inversion can be performed.

Monthly Notices of the Royal Astronomical SocietyVol. 548(4)
Rutherford Appleton Laboratory (GB), United States Naval Research Laboratory (US), University of Helsinki (FI), University of Zagreb (HR), Helsinki Institute of Physics (FI), Johns Hopkins University Applied Physics Laboratory (US), Graz University of Technology (AT), Space Research Institute (AT), Predictive Science (United States) (US), University of Reading (GB)
National Science Foundation, National Aeronautics and Space Administration, European Commission, Austrian Science Fund, Science and Technology Facilities Council, Office of Advanced Cyberinfrastructure, Rutherford Appleton Laboratory, H2020 European Research Council, International Space Science Institute
Openalex Percentile: Top 10%
Solar and Space Plasma Dynamics
AI Navigator

Ask Laika to Summarize, Analyze, and Connect papers live on the map.

Summarize Papers & Methodologies

Extract key findings, datasets, and comparative methods across publications.

Benchmark Rankings & Visual Analytics

Rank top research institutions, authors, funders, topics, and journals by Field-Weighted Citation Impact (FWCI) and paper volume with instant charts.

Connect Distant Disciplines

Bridge topological clusters on the map to find hidden collaborative intersections.