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1. Identity statement
Reference TypeJournal Article
Siteplutao.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
IdentifierJ8LNKAN8RW/3C63KPG
Repositorydpi.inpe.br/plutao/2012/06.21.18.26.20   (restricted access)
Last Update2012:08.24.19.37.12 (UTC) administrator
Metadata Repositorydpi.inpe.br/plutao/2012/06.21.18.26.21
Metadata Last Update2021:02.11.18.11.12 (UTC) administrator
DOI10.1155/2012/905209
ISSN1024-123X
1563-5147
Labellattes: 7340081273816424 2 SukhanovPrad:2012:LoOrTr
Citation KeySukhanovPrad:2012:LoOrTr
TitleLow-Thrust Orbital Transfers in the Two-Body Problem
Year2012
Access Date2024, Apr. 18
Secondary TypePRE PI
Number of Files1
Size2225 KiB
2. Context
Author1 Sukhanov, A. A.
2 Prado, Antonio Fernando Bertachini de Almeida
Resume Identifier1
2 8JMKD3MGP5W/3C9JGJA
Group1
2 DMC-ETE-INPE-MCTI-GOV-BR
Affiliation1 Space Research Institute (IKI), RAS, Moscow, Russia
2 Instituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Address1
2 abertachini@terra.com.br
e-Mail Addressabertachini@terra.com.br
JournalMathematical Problems in Engineering
Volume2012
NumberArticle ID 905209
Pages1-20
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 00:10:59 :: lattes -> administrator :: 2012
2012-07-21 01:08:35 :: administrator -> secretaria.cpa@dir.inpe.br :: 2012
2012-11-29 13:50:22 :: secretaria.cpa@dir.inpe.br -> administrator :: 2012
2021-02-11 18:11:12 :: administrator -> marciana :: 2012
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsAstrodinâmica
Manobras Orbitais
Trajetórias Espaciais
AbstractLow-thrust transfers between given orbits within the two-body problem are considered; the thrust is assumed power limited. A simple method for obtaining the transfer trajectories based on the linearization of the motion near reference orbits is suggested. Required calculation accuracy can be reached by means of use of a proper number of the reference orbits. The method may be used in the case of a large number of the orbits around the attracting center; no averaging is necessary in this case. The suggested method also is applicable to the cases of partly given final orbit and if there are constraints on the thrust direction. The method gives an optimal solution to the linearized problem which is not optimal for the original nonlinear problem; the difference between the optimal solutions to the original and linearized problems is estimated using a numerical example. Also examples illustrating the method capacities are given.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Low-Thrust Orbital Transfers...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
Languageen
Target FileSukhanov&Prado_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
DisseminationPORTALCAPES
Host Collectiondpi.inpe.br/plutao@80/2008/08.19.15.01
6. Notes
Empty Fieldsalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel format isbn lineage mark mirrorrepository month nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject tertiarymark tertiarytype typeofwork url
7. Description control
e-Mail (login)marciana
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