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Physics-Inspired Machine Learning for orbit determination in Low-Earth Orbit

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Resumo:We have always been told since we were little that space is infinite. Having this in mind, it would not make much sense to be so cautious and aware of the space that lies above us. However, the area right above the Earth’s surface up to 2000 km is heavily contaminated with space debris which can have all kinds of origins and dimensions both man-made (inactive satellites, parts of rockets, minuscule flecks of paint) as well as from natural sources (small meteoroids). Considering that satellites have their propellant carefully measured to fulfill the planned trajectory and cannot afford evasion maneuvers at the slightest danger signal, it is important to quantify the uncertainty on the predictions made. To predict when two objects will collide, one will need to model their orbits with the goal of knowing their positions. Among the multiple elements involved, such as the gravity potential or the shape of the object, space weather is the most difficult to predict. Because of these stochastic variables, the early discoveries from multiple scientists in the eighteenth century were only enough to describe an orbit in the perfect case scenario. These variables make the modeling of a real orbit more challenging since they are random and have to be considered when modeling them since their effects are not negligible. One of the variables that has the most impact on calculating the orbit of a space object is atmospheric density. Since we are dealing with a physical system that abides by physical laws, even if not perfectly, this will be used to our advantage to improve the predictions made. As aforementioned, these laws known for centuries can be too tailored for the perfect-case scenario and new equations can be discovered to better model a real-case scenario. The objective of this research is to employ physically informed machine learning techniques for orbit determination as well as to model atmospheric density by leveraging physical domain knowledge and improving upon the standard approach.
Autores principais:Funenga, João Pedro de Noronha
Assunto:Physically-Informed Neural Networks Data-driven physical discovery Space Debris Orbital Mechanics Orbit determination
Ano:2023
País:Portugal
Tipo de documento:dissertação de mestrado
Tipo de acesso:acesso aberto
Instituição associada:Universidade Nova de Lisboa
Idioma:inglês
Origem:Repositório Institucional da UNL
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author Funenga, João Pedro de Noronha
author_facet Funenga, João Pedro de Noronha
author_role author
contributor_name_str_mv Soares, Cláudia
Guimarães, Marta
Costa, Henrique
RUN
country_str PT
creators_json_txt [{\"Person.name\":\"Funenga, João Pedro de Noronha\"}]
datacite.contributors.contributor.contributorName.fl_str_mv Soares, Cláudia
Guimarães, Marta
Costa, Henrique
RUN
datacite.creators.creator.creatorName.fl_str_mv Funenga, João Pedro de Noronha
datacite.date.Accepted.fl_str_mv 2023-12-01T00:00:00Z
datacite.date.available.fl_str_mv 2024-03-05T18:41:04Z
datacite.date.embargoed.fl_str_mv 2024-03-05T18:41:04Z
datacite.rights.fl_str_mv http://purl.org/coar/access_right/c_abf2
datacite.subjects.subject.fl_str_mv Physically-Informed Neural Networks
Data-driven physical discovery
Space Debris
Orbital Mechanics
Orbit determination
datacite.titles.title.fl_str_mv Physics-Inspired Machine Learning for orbit determination in Low-Earth Orbit
dc.contributor.none.fl_str_mv Soares, Cláudia
Guimarães, Marta
Costa, Henrique
RUN
dc.creator.none.fl_str_mv Funenga, João Pedro de Noronha
dc.date.Accepted.fl_str_mv 2023-12-01T00:00:00Z
dc.date.available.fl_str_mv 2024-03-05T18:41:04Z
dc.date.embargoed.fl_str_mv 2024-03-05T18:41:04Z
dc.format.none.fl_str_mv application/pdf
dc.identifier.none.fl_str_mv http://hdl.handle.net/10362/164463
dc.language.none.fl_str_mv eng
dc.rights.none.fl_str_mv http://purl.org/coar/access_right/c_abf2
dc.subject.none.fl_str_mv Physically-Informed Neural Networks
Data-driven physical discovery
Space Debris
Orbital Mechanics
Orbit determination
dc.title.fl_str_mv Physics-Inspired Machine Learning for orbit determination in Low-Earth Orbit
dc.type.none.fl_str_mv http://purl.org/coar/resource_type/c_bdcc
description We have always been told since we were little that space is infinite. Having this in mind, it would not make much sense to be so cautious and aware of the space that lies above us. However, the area right above the Earth’s surface up to 2000 km is heavily contaminated with space debris which can have all kinds of origins and dimensions both man-made (inactive satellites, parts of rockets, minuscule flecks of paint) as well as from natural sources (small meteoroids). Considering that satellites have their propellant carefully measured to fulfill the planned trajectory and cannot afford evasion maneuvers at the slightest danger signal, it is important to quantify the uncertainty on the predictions made. To predict when two objects will collide, one will need to model their orbits with the goal of knowing their positions. Among the multiple elements involved, such as the gravity potential or the shape of the object, space weather is the most difficult to predict. Because of these stochastic variables, the early discoveries from multiple scientists in the eighteenth century were only enough to describe an orbit in the perfect case scenario. These variables make the modeling of a real orbit more challenging since they are random and have to be considered when modeling them since their effects are not negligible. One of the variables that has the most impact on calculating the orbit of a space object is atmospheric density. Since we are dealing with a physical system that abides by physical laws, even if not perfectly, this will be used to our advantage to improve the predictions made. As aforementioned, these laws known for centuries can be too tailored for the perfect-case scenario and new equations can be discovered to better model a real-case scenario. The objective of this research is to employ physically informed machine learning techniques for orbit determination as well as to model atmospheric density by leveraging physical domain knowledge and improving upon the standard approach.
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person_str_mv Funenga, João Pedro de Noronha
publishDate 2023
repo_facet_str urn:repositoryAcronym:run{{{_:::_}}}Repositório Institucional da UNL
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spelling engpt_PTWe have always been told since we were little that space is infinite. Having this in mind, it would not make much sense to be so cautious and aware of the space that lies above us. However, the area right above the Earth’s surface up to 2000 km is heavily contaminated with space debris which can have all kinds of origins and dimensions both man-made (inactive satellites, parts of rockets, minuscule flecks of paint) as well as from natural sources (small meteoroids). Considering that satellites have their propellant carefully measured to fulfill the planned trajectory and cannot afford evasion maneuvers at the slightest danger signal, it is important to quantify the uncertainty on the predictions made. To predict when two objects will collide, one will need to model their orbits with the goal of knowing their positions. Among the multiple elements involved, such as the gravity potential or the shape of the object, space weather is the most difficult to predict. Because of these stochastic variables, the early discoveries from multiple scientists in the eighteenth century were only enough to describe an orbit in the perfect case scenario. These variables make the modeling of a real orbit more challenging since they are random and have to be considered when modeling them since their effects are not negligible. One of the variables that has the most impact on calculating the orbit of a space object is atmospheric density. Since we are dealing with a physical system that abides by physical laws, even if not perfectly, this will be used to our advantage to improve the predictions made. As aforementioned, these laws known for centuries can be too tailored for the perfect-case scenario and new equations can be discovered to better model a real-case scenario. The objective of this research is to employ physically informed machine learning techniques for orbit determination as well as to model atmospheric density by leveraging physical domain knowledge and improving upon the standard approach.application/pdfpt_PTPhysics-Inspired Machine Learning for orbit determination in Low-Earth OrbitFunenga, João Pedro de NoronhaSoares, CláudiaGuimarães, MartaCosta, HenriqueHostingInstitutionOrganizationalRUNe-mailmailto:run@unl.ptrun@unl.pt2024-03-05T18:41:04Z2023-122023-12-01T00:00:00ZHandlehttp://hdl.handle.net/10362/164463http://purl.org/coar/access_right/c_abf2open accessPhysically-Informed Neural NetworksData-driven physical discoverySpace DebrisOrbital MechanicsOrbit determination12778753 bytesliteraturehttp://purl.org/coar/resource_type/c_bdccmaster thesishttp://purl.org/coar/access_right/c_abf2application/pdffulltexthttps://run.unl.pt/bitstreams/0d78014b-597f-4f3a-a3b8-edae88f3f4a1/download
spellingShingle Physics-Inspired Machine Learning for orbit determination in Low-Earth Orbit
Funenga, João Pedro de Noronha
Physically-Informed Neural Networks
Data-driven physical discovery
Space Debris
Orbital Mechanics
Orbit determination
status SINGLETON
subject.fl_str_mv Physically-Informed Neural Networks
Data-driven physical discovery
Space Debris
Orbital Mechanics
Orbit determination
title Physics-Inspired Machine Learning for orbit determination in Low-Earth Orbit
title_full Physics-Inspired Machine Learning for orbit determination in Low-Earth Orbit
title_fullStr Physics-Inspired Machine Learning for orbit determination in Low-Earth Orbit
title_full_unstemmed Physics-Inspired Machine Learning for orbit determination in Low-Earth Orbit
title_short Physics-Inspired Machine Learning for orbit determination in Low-Earth Orbit
title_sort Physics-Inspired Machine Learning for orbit determination in Low-Earth Orbit
topic Physically-Informed Neural Networks
Data-driven physical discovery
Space Debris
Orbital Mechanics
Orbit determination
topic_facet Physically-Informed Neural Networks
Data-driven physical discovery
Space Debris
Orbital Mechanics
Orbit determination
url http://hdl.handle.net/10362/164463
visible 1