Power simulation of a CubeSat: influence of orbit, attitude and thermal control
Main Author: | |
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Publication Date: | 2023 |
Other Authors: | , , |
Format: | Article |
Language: | eng |
Source: | Repositório Institucional da UNESP |
Download full: | http://dx.doi.org/10.1109/LES.2023.3250101 http://hdl.handle.net/11449/246936 |
Summary: | CubeSats must endure the extreme temperature and radiation changes that are a result of the environment in orbit. The power system of CubeSats, which produces the electrical energy required to carry out the activities, is a crucial component. The photovoltaic effect, a phenomenon whose maximum power point decreases as temperature rises while the peak rises with solar radiation intensity rises, is used by the majority of satellites, including CubeSats, to convert solar radiation into electrical energy. High temperatures should be avoided since they decrease the effectiveness of this photovoltaic phenomenon, whereas high solar radiation levels are required to produce more energy. This study evaluates a simulation of a CubeSat 1U with solar panels mounted on all of its faces to examine the impact of orbit, attitude, and temperature management on power generation. The outcomes show that higher performance may be obtained by carefully choosing these factors. |
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Power simulation of a CubeSat: influence of orbit, attitude and thermal controlCubesatCubeSatOrbitsPhotovoltaic CellPower GenerationSimulationSolar PanelSolar panelsSolar radiationSpace heatingSpace vehiclesSunCubeSats must endure the extreme temperature and radiation changes that are a result of the environment in orbit. The power system of CubeSats, which produces the electrical energy required to carry out the activities, is a crucial component. The photovoltaic effect, a phenomenon whose maximum power point decreases as temperature rises while the peak rises with solar radiation intensity rises, is used by the majority of satellites, including CubeSats, to convert solar radiation into electrical energy. High temperatures should be avoided since they decrease the effectiveness of this photovoltaic phenomenon, whereas high solar radiation levels are required to produce more energy. This study evaluates a simulation of a CubeSat 1U with solar panels mounted on all of its faces to examine the impact of orbit, attitude, and temperature management on power generation. The outcomes show that higher performance may be obtained by carefully choosing these factors.Federal University of Maranhão, MA, BrazilSão Paulo State University, SP, BrazilUniversity of Vale do Itajaí, SC, Brazil2023-07-29T12:54:36Z2023-07-29T12:54:36Z2023-01-01info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/articlehttp://dx.doi.org/10.1109/LES.2023.3250101IEEE Embedded Systems Letters.1943-06711943-0663http://hdl.handle.net/11449/24693610.1109/LES.2023.32501012-s2.0-85149371748Scopusreponame:Repositório Institucional da UNESPinstname:Universidade Estadual Paulista (UNESP)instacron:UNESPengIEEE Embedded Systems LettersSantana, Andre L. RodriguesFilho, Edemar Morschde Souza, Francisco das ChagasSeman, Laio O.info:eu-repo/semantics/openAccess2023-07-29T12:54:36Zoai:repositorio.unesp.br:11449/246936Repositório InstitucionalPUBhttp://repositorio.unesp.br/oai/requestrepositoriounesp@unesp.bropendoar:29462025-03-28T15:07:56.341417Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)false |
dc.title.none.fl_str_mv |
Power simulation of a CubeSat: influence of orbit, attitude and thermal control |
title |
Power simulation of a CubeSat: influence of orbit, attitude and thermal control |
spellingShingle |
Power simulation of a CubeSat: influence of orbit, attitude and thermal control Santana, Andre L. Rodrigues Cubesat CubeSat Orbits Photovoltaic Cell Power Generation Simulation Solar Panel Solar panels Solar radiation Space heating Space vehicles Sun |
title_short |
Power simulation of a CubeSat: influence of orbit, attitude and thermal control |
title_full |
Power simulation of a CubeSat: influence of orbit, attitude and thermal control |
title_fullStr |
Power simulation of a CubeSat: influence of orbit, attitude and thermal control |
title_full_unstemmed |
Power simulation of a CubeSat: influence of orbit, attitude and thermal control |
title_sort |
Power simulation of a CubeSat: influence of orbit, attitude and thermal control |
author |
Santana, Andre L. Rodrigues |
author_facet |
Santana, Andre L. Rodrigues Filho, Edemar Morsch de Souza, Francisco das Chagas Seman, Laio O. |
author_role |
author |
author2 |
Filho, Edemar Morsch de Souza, Francisco das Chagas Seman, Laio O. |
author2_role |
author author author |
dc.contributor.author.fl_str_mv |
Santana, Andre L. Rodrigues Filho, Edemar Morsch de Souza, Francisco das Chagas Seman, Laio O. |
dc.subject.por.fl_str_mv |
Cubesat CubeSat Orbits Photovoltaic Cell Power Generation Simulation Solar Panel Solar panels Solar radiation Space heating Space vehicles Sun |
topic |
Cubesat CubeSat Orbits Photovoltaic Cell Power Generation Simulation Solar Panel Solar panels Solar radiation Space heating Space vehicles Sun |
description |
CubeSats must endure the extreme temperature and radiation changes that are a result of the environment in orbit. The power system of CubeSats, which produces the electrical energy required to carry out the activities, is a crucial component. The photovoltaic effect, a phenomenon whose maximum power point decreases as temperature rises while the peak rises with solar radiation intensity rises, is used by the majority of satellites, including CubeSats, to convert solar radiation into electrical energy. High temperatures should be avoided since they decrease the effectiveness of this photovoltaic phenomenon, whereas high solar radiation levels are required to produce more energy. This study evaluates a simulation of a CubeSat 1U with solar panels mounted on all of its faces to examine the impact of orbit, attitude, and temperature management on power generation. The outcomes show that higher performance may be obtained by carefully choosing these factors. |
publishDate |
2023 |
dc.date.none.fl_str_mv |
2023-07-29T12:54:36Z 2023-07-29T12:54:36Z 2023-01-01 |
dc.type.status.fl_str_mv |
info:eu-repo/semantics/publishedVersion |
dc.type.driver.fl_str_mv |
info:eu-repo/semantics/article |
format |
article |
status_str |
publishedVersion |
dc.identifier.uri.fl_str_mv |
http://dx.doi.org/10.1109/LES.2023.3250101 IEEE Embedded Systems Letters. 1943-0671 1943-0663 http://hdl.handle.net/11449/246936 10.1109/LES.2023.3250101 2-s2.0-85149371748 |
url |
http://dx.doi.org/10.1109/LES.2023.3250101 http://hdl.handle.net/11449/246936 |
identifier_str_mv |
IEEE Embedded Systems Letters. 1943-0671 1943-0663 10.1109/LES.2023.3250101 2-s2.0-85149371748 |
dc.language.iso.fl_str_mv |
eng |
language |
eng |
dc.relation.none.fl_str_mv |
IEEE Embedded Systems Letters |
dc.rights.driver.fl_str_mv |
info:eu-repo/semantics/openAccess |
eu_rights_str_mv |
openAccess |
dc.source.none.fl_str_mv |
Scopus reponame:Repositório Institucional da UNESP instname:Universidade Estadual Paulista (UNESP) instacron:UNESP |
instname_str |
Universidade Estadual Paulista (UNESP) |
instacron_str |
UNESP |
institution |
UNESP |
reponame_str |
Repositório Institucional da UNESP |
collection |
Repositório Institucional da UNESP |
repository.name.fl_str_mv |
Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP) |
repository.mail.fl_str_mv |
repositoriounesp@unesp.br |
_version_ |
1834483050565599232 |