Single-spacecraft techniques for shock parameters estimation: A systematic approach

dc.contributor.authorTrotta Domenico
dc.contributor.authorVuorinen Laura
dc.contributor.authorHietala Heli
dc.contributor.authorHorbury Tim
dc.contributor.authorDresing Nina
dc.contributor.authorGieseler Jan
dc.contributor.authorKouloumvakos Athanasios
dc.contributor.authorPrice Daniel
dc.contributor.authorValentini Francesco
dc.contributor.authorKilpua Emilia
dc.contributor.authorVainio Rami
dc.contributor.organizationfi=avaruustutkimuslaboratorio|en=Space Research Laboratory|
dc.contributor.organizationfi=fysiikan ja tähtitieteen laitos|en=Department of Physics and Astronomy|
dc.contributor.organization-code1.2.246.10.2458963.20.47833719389
dc.contributor.organization-code1.2.246.10.2458963.20.55477946762
dc.converis.publication-id176640697
dc.converis.urlhttps://research.utu.fi/converis/portal/Publication/176640697
dc.date.accessioned2022-10-28T13:40:33Z
dc.date.available2022-10-28T13:40:33Z
dc.description.abstract<p>Spacecraft missions provide the unique opportunity to study the properties of collisionless shocks utilising <em>in situ</em> measurements. In the past years, several diagnostics have been developed to address key shock parameters using time series of magnetic field (and plasma) data collected by a single spacecraft crossing a shock front. A critical aspect of such diagnostics is the averaging process involved in the evaluation of upstream/downstream quantities. In this work, we discuss several of these techniques, with a particular focus on the shock obliquity (defined as the angle between the upstream magnetic field and the shock normal vector) estimation. We introduce a systematic variation of the upstream/downstream averaging windows, yielding to an ensemble of shock parameters, which is a useful tool to address the robustness of their estimation. This approach is first tested with a synthetic shock dataset compliant with the Rankine-Hugoniot jump conditions for a shock, including the presence of noise and disturbances. We then employ self-consistent, hybrid kinetic shock simulations to apply the diagnostics to virtual spacecraft crossing the shock front at various stages of its evolution, highlighting the role of shock-induced fluctuations in the parameters’ estimation. This approach has the strong advantage of retaining some important properties of collisionless shock (such as, for example, the shock front microstructure) while being able to set a known, nominal set of shock parameters. Finally, two recent observations of interplanetary shocks from the Solar Orbiter spacecraft are presented, to demonstrate the use of this systematic approach to real events of shock crossings. The approach is also tested on an interplanetary shock measured by the four spacecraft of the Magnetospheric Multiscale (MMS) mission. All the Python software developed and used for the diagnostics (SerPyShock) is made available for the public, including an example of parameter estimation for a shock wave recently observed <em>in-situ</em> by the Solar Orbiter spacecraft.<br></p>
dc.identifier.eissn2296-987X
dc.identifier.jour-issn2296-987X
dc.identifier.olddbid183544
dc.identifier.oldhandle10024/166638
dc.identifier.urihttps://www.utupub.fi/handle/11111/40817
dc.identifier.urlhttps://www.frontiersin.org/articles/10.3389/fspas.2022.1005672/full
dc.identifier.urnURN:NBN:fi-fe2022102463113
dc.language.isoen
dc.okm.affiliatedauthorVuorinen, Laura
dc.okm.affiliatedauthorGieseler, Nina
dc.okm.affiliatedauthorGieseler, Jan
dc.okm.affiliatedauthorVainio, Rami
dc.okm.discipline115 Astronomy and space scienceen_GB
dc.okm.discipline115 Avaruustieteet ja tähtitiedefi_FI
dc.okm.internationalcopublicationinternational co-publication
dc.okm.internationalityInternational publication
dc.okm.typeA1 ScientificArticle
dc.publisherFrontiers Research Foundation
dc.publisher.countrySwitzerlanden_GB
dc.publisher.countrySveitsifi_FI
dc.publisher.country-codeCH
dc.relation.doi10.3389/fspas.2022.1005672
dc.relation.ispartofjournalFrontiers in Astronomy and Space Sciences
dc.source.identifierhttps://www.utupub.fi/handle/10024/166638
dc.titleSingle-spacecraft techniques for shock parameters estimation: A systematic approach
dc.year.issued2022

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