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1. Identity statement
Reference TypeJournal Article
Sitemtc-m21b.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34P/3MRJQ92
Repositorysid.inpe.br/mtc-m21b/2016/11.22.18.27   (restricted access)
Last Update2016:11.22.18.27.23 (UTC) simone
Metadata Repositorysid.inpe.br/mtc-m21b/2016/11.22.18.27.23
Metadata Last Update2018:06.04.02.41.21 (UTC) administrator
DOI10.1007/s40314-016-0331-y
ISSN2238-3603
Citation KeyZanardiOrlMotPelSil:2016:NuAnAp
TitleNumerical and analytical approach for the spin-stabilized satellite attitude propagation
Year2016
MonthOct.
Access Date2024, May 19
Type of Workjournal article
Secondary TypePRE PN
Number of Files1
Size1242 KiB
2. Context
Author1 Zanardi, M. Cecília
2 Orlando, Valcir
3 Motta, Gabriel Bordores
4 Pelosi, Tatiane
5 Silva, William Reis
Resume Identifier1
2 8JMKD3MGP5W/3C9JJAL
Group1
2 CRC-CRC-INPE-MCTI-GOV-BR
Affiliation1 Universidade Federal do ABC (UFABC)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 Universidade Estadual Paulista (UNESP)
4 Universidade Estadual Paulista (UNESP)
5 Universidade Estadual Paulista (UNESP)
Author e-Mail Address1 mceciliazanardi@gmail.com
2 valcir@ccs.inpe.br
3 gabriel_borderes@yahoo.com.br
4 tatiane.pelosi@gmail.com
5 reis.william@gmail.com
JournalComputational and Applied Mathematics
Volume35
Number3
Pages937-949
Secondary MarkB2_MATEMÁTICA_/_PROBABILIDADE_E_ESTATÍSTICA B2_INTERDISCIPLINAR B3_CIÊNCIA_DA_COMPUTAÇÃO B4_ENGENHARIAS_IV
History (UTC)2016-11-22 18:28:07 :: simone -> administrator :: 2016
2018-06-04 02:41:21 :: administrator -> simone :: 2016
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsAttitude prediction
Euler angles
External torques
Quaternion
Spin axis
AbstractThis paper presents the comparison between the numerical and analytical results of a spacecraft attitude propagation for a spin-stabilized satellite. Some external torques are introduced in the equations of the motion and the comparisons are done considering that these torques are acting together, which are: gravity gradient, aerodynamic, solar radiation, magnetic residual and eddy current. In the numerical approach it is used the quaternion to represent the attitude. This numerical approach can be applied for any kind of satellite. The analytical approach is applied directly for a spin-stabilized satellite and the equations of motion are described in terms of the spin velocity, spin axis right ascension and declination angles. An analytical solution of these equations is presented and valid for one orbit period. Applications are developed considering the Brazilian spin-stabilized satellites SCD1 and SCD2. The comparisons are important to validate some simplifications that are required in the analytical approach. The results show that the average components of the external torque are sufficient to observe the main influence of the considered torques.
AreaETES
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4. Conditions of access and use
Languageen
Target Filezanardi_numerical.pdf
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Update Permissionnot transferred
5. Allied materials
Mirror Repositoryurlib.net/www/2011/03.29.20.55
Next Higher Units8JMKD3MGPCW/3F3PAJE
Citing Item Listsid.inpe.br/bibdigital/2013/10.19.00.29 6
sid.inpe.br/mtc-m21/2012/07.13.15.01.12 1
DisseminationPORTALCAPES
Host Collectionsid.inpe.br/mtc-m21b/2013/09.26.14.25.20
6. Notes
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