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1. Identity statement
Reference TypeJournal Article
Siteplutao.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
IdentifierJ8LNKAN8RW/3C649BC
Repositorydpi.inpe.br/plutao/2012/06.21.21.47.25   (restricted access)
Last Update2012:08.24.17.34.41 (UTC) administrator
Metadata Repositorydpi.inpe.br/plutao/2012/06.21.21.47.26
Metadata Last Update2021:02.11.18.11.14 (UTC) administrator
DOI10.1155/2012/137672
ISSN1024-123X
1563-5147
Labellattes: 3638759062433933 5 ReisSilvaZanCabForFor:2012:StStRo
Citation KeyReisSilvaZanaCabeForm:2012:StStRo
TitleStudy of Stability of Rotational Motion of Spacecraft with Canonical Variables
Year2012
Access Date2024, Apr. 18
Secondary TypePRE PI
Number of Files1
Size1071 KiB
2. Context
Author1 Reis Silva, William
2 Zanardi, Maria Cecília F. P. S.
3 Cabette, Regina Elaine Santos
4 Formiga, Jorge Kennety Silva
Group1
2
3 DMC-ETE-INPE-MCTI-GOV-BR
Affiliation1 Sao Paulo State University (UNESP) Guaratinguetá
2 Sao Paulo Salesian University (UNISAL)
3 Instituto Nacional de Pesquisas Espaciais (INPE)
4 Faculty of Technology (FATEC), Sao Jose dos Campos
Author e-Mail Address1 reis.william@gmail.com
2
3
4 jkennety@yahoo.com.br
e-Mail Addressjkennety@yahoo.com.br
JournalMathematical Problems in Engineering
Volume2012
NumberID-137672
Pages1-19
Secondary MarkB5_ASTRONOMIA_/_FÍSICA B4_CIÊNCIA_DA_COMPUTAÇÃO B3_CIÊNCIAS_AGRÁRIAS_I B1_ENGENHARIAS_I B2_ENGENHARIAS_II B1_ENGENHARIAS_III A2_ENGENHARIAS_IV A2_INTERDISCIPLINAR B3_MATEMÁTICA_/_PROBABILIDADE_E_ESTATÍSTICA
History (UTC)2012-06-22 00:11:01 :: lattes -> administrator :: 2012
2012-07-21 11:59:03 :: administrator -> secretaria.cpa@dir.inpe.br :: 2012
2012-08-24 17:34:41 :: secretaria.cpa@dir.inpe.br -> administrator :: 2012
2021-02-11 18:11:14 :: administrator -> marciana :: 2012
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
AbstractThiswork aims to analyze the stability of the rotational motion of artificial satellites in circular orbit with the influence of gravity gradient torque, using the Andoyer variables. The used method in this paper to analyze stability is the Kovalev-Savchenko theorem. This method requires the reduction of the Hamiltonian in its normal form up to fourth order by means of canonical transformations around equilibrium points. The coefficients of the normal Hamiltonian are indispensable in the study of nonlinear stability of its equilibrium points according to the three established conditions in the theorem. Some physical and orbital data of real satellites were used in the numerical simulations. In comparison with previous work, the results show a greater number of equilibrium points and an optimization in the algorithm to determine the normal form and stability analysis. The results of this paper can directly contribute in maintaining the attitude of artificial satellites.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Study of Stability...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
Languageen
Target FileReisSilva_et_al_2012.pdf
User Groupadministrator
lattes
secretaria.cpa@dir.inpe.br
Visibilityshown
Archiving Policydenypublisher allowfinaldraft
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Next Higher Units8JMKD3MGPCW/446AF4B
URL (untrusted data)http://www.hindawi.com/journals/mpe/2012/137672/
DisseminationPORTALCAPES
Host Collectiondpi.inpe.br/plutao@80/2008/08.19.15.01
6. Notes
Empty Fieldsalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel format isbn keywords lineage mark mirrorrepository month nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup resumeid rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject tertiarymark tertiarytype typeofwork
7. Description control
e-Mail (login)marciana
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