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1. Identity statement
Reference TypeJournal Article
Sitemtc-m21d.sid.inpe.br (namespace prefix: upn:44QHRCS)
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34T/46PR3BE
Repositorysid.inpe.br/mtc-m21d/2022/04.27.18.56
Last Update2022:04.27.18.56.34 (UTC) simone
Metadata Repositorysid.inpe.br/mtc-m21d/2022/04.27.18.56.34
Metadata Last Update2023:01.04.16.16.04 (UTC) simone
DOI10.22201/ia.01851101p.2022.58.01.02
ISSN0185-1101
Citation KeyMeirelesPradMeloPere:2022:StDiAt
TitleA study on different attitude strategies and mission parameters based on lightsail-2
Year2022
MonthApr.
Access Date2025, Dec. 08
Type of Workjournal article
Secondary TypePRE PI
Number of Files1
Size938 KiB
2. Context
Author1 Meireles, Lucas Gouvêa
2 Prado, Antonio Fernando Bertachini de Almeida
3 Melo, C. de
4 Pereira, M. C.
Resume Identifier1
2 8JMKD3MGP5W/3C9JGJA
Group1 CMC-ETES-DIPGR-INPE-MCTI-GOV-BR
2 DIMEC-CGCE-INPE-MCTI-GOV-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 Universidade Federal de Minas Gerais (UFMG)
4 Universidade Federal de Minas Gerais (UFMG)
Author e-Mail Address1 meireleslg@gmail.com
2 antonio.prado@inpe.br
JournalRevista Mexicana de Astronomia y Astrofisica
Volume58
Number1
Pages23-35
Secondary MarkB1_ASTRONOMIA_/_FÍSICA
Host Collectionurlib.net/www/2021/06.04.03.40 upn:44QHRCS
History (UTC)2022-04-27 18:56:34 :: simone -> administrator ::
2022-04-27 18:56:35 :: administrator -> simone :: 2022
2022-04-27 18:56:56 :: simone -> administrator :: 2022
2023-01-03 16:46:05 :: administrator -> simone :: 2022
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
Keywordscelestial mechanics
methods
numerical
minor planets
asteroids
general
space vehicles
AbstractThe Planetary Society's LightSail-2 mission successfully validated the orbital maneuvering capability of a solar radiation pressure (SRP) propelled spacecraft. This paper presents a study on two alternative attitude strategies for the orientation of a solar sail. The goal is to increase the effect of the SRP acceleration over the spacecraft's orbital trajectory, with the intention of maintaining or even gaining altitude over time. Furthermore, one of these strategies was employed while varying a few of the mission's parameters to determine if it would be viable to maintain the spacecraft's average altitude. Results show that it is possible to increase the average altitude of the spacecraft over time while still reducing the number of maneuvers necessary to change the spacecraft's attitude. With that result in hand, it is also possible to change some of the mission parameters without compromising the solar sailing performance.
AreaETES
Arrangement 1urlib.net > BDMCI > Fonds > Produção pgr ATUAIS > CMC > A study on...
Arrangement 2urlib.net > BDMCI > Fonds > Produção a partir de 2021 > CGCE > A study on...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Content
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4. Conditions of access and use
data URIupn:44QHRCS:8JMKD3MGP3W34T/46PR3BE
data URLhttp://urlib.net/ibi/8JMKD3MGP3W34T/46PR3BE
zipped data URLhttp://urlib.net/zip/8JMKD3MGP3W34T/46PR3BE
Languageen
Target Filemeireles_2022.pdf
User Groupsimone
Reader Groupadministrator
simone
Visibilityshown
Archiving Policyallowpublisher allowfinaldraft
Update Permissionnot transferred
5. Allied materials
Next Higher Units8JMKD3MGPCW/3F2UALS
8JMKD3MGPCW/46KTFK8
Citing Item Listsid.inpe.br/bibdigital/2013/10.14.00.13 - 46
sid.inpe.br/bibdigital/2022/04.03.17.52 - 41
sid.inpe.br/mtc-m21/2012/07.13.14.40.20 - 7
DisseminationWEBSCI; PORTALCAPES; SCIELO; SCOPUS.
6. Notes
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