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1. Identity statement
Reference TypeJournal Article
Sitemtc-m21c.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34R/3RPHKMD
Repositorysid.inpe.br/mtc-m21c/2018/09.05.12.02.53   (restricted access)
Last Update2018:09.05.12.02.53 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m21c/2018/09.05.12.02.54
Metadata Last Update2021:03.30.19.37.21 (UTC) administrator
DOI10.1007/s10509-018-3400-4
ISSN0004-640X
Citation KeySmirnovMasOvcShePra:2018:TeFoNa
TitleTetrahedron formation of nanosatellites with single-input control
Year2018
MonthSept.
Access Date2024, May 08
Type of Workjournal article
Secondary TypePRE PI
Number of Files1
Size992 KiB
2. Context
Author1 Smirnov, G. V.
2 Mashtakov, Y.
3 Ovchinnikov, M.
4 Shestakov, S.
5 Prado, Antonio Fernando Bertachini de Almeida
Resume Identifier1
2
3
4
5 8JMKD3MGP5W/3C9JGJA
Group1
2
3
4
5 DMC-ETE-INPE-MCTI-GOV-BR
Affiliation1
2
3
4
5 Instituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Address1 smirnov@math.uminho.pt
2
3
4
5 antonio.prado@inpe.br
JournalAstrophysics and Space Science
Volume363
Number9
Pagese180
Secondary MarkB1_GEOCIÊNCIAS B3_MATEMÁTICA_/_PROBABILIDADE_E_ESTATÍSTICA B3_ASTRONOMIA_/_FÍSICA
History (UTC)2018-09-05 12:02:54 :: simone -> administrator ::
2021-03-30 19:37:21 :: administrator -> simone :: 2018
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsFormation flying
Single-input control
Tetrahedral formation
AbstractThe present paper studies the formation flight of four nanosatellites forming a tetrahedron. The main goal of this research is to find the relative orbits of these satellites that, at least in the linear Hill-Clohessy-Wiltshire model, ensure finite relative motion and keep the volume and shape of the tetrahedron configuration. Since real motions of these satellites will differ from the linear ones, especially under the influence of the perturbation, active control is necessary. In addition, the limited size of the satellites does not allow us to use a complex 3-axis attitude control system. In the present paper we consider the passive magnetic attitude control system and suppose that the thrust direction is always aligned with the local geomagnetic field. In order to increase mission lifetime the control algorithm that minimizes the propellant consumption and keeps the tetrahedron volume and shape is investigated.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Tetrahedron formation of...
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4. Conditions of access and use
Languageen
Target FileSmirnov__Tetrahedron.pdf
User Groupsimone
Visibilityshown
Archiving Policydenypublisher denyfinaldraft12
Read Permissiondeny from all
Update Permissionnot transferred
5. Allied materials
Next Higher Units8JMKD3MGPCW/446AF4B
DisseminationWEBSCI; PORTALCAPES.
Host Collectionurlib.net/www/2017/11.22.19.04
6. Notes
Empty Fieldsalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress format isbn label lineage mark mirrorrepository nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject tertiarymark tertiarytype url
7. Description control
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