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1. Identity statement
Reference TypeBook Section
Sitemarte3.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier6qtX3pFwXQZ3r59YCT/H3JSj
Repositorysid.inpe.br/iris@1905/2005/08.04.02.05   (restricted access)
Last Update2019:01.16.16.20.00 (UTC) simone
Metadata Repositorysid.inpe.br/iris@1905/2005/08.04.02.05.25
Metadata Last Update2021:02.11.18.10.09 (UTC) administrator
Secondary KeyINPE-9537-PRE/5190
Label10465
Citation KeyJesusSouzPrad:2002:SuPrOr
TitleA survey on the problem of orbital maneuvers for an artificial satellite
FormatISBN 85-17-00006-4
Year2002
Secondary Date20021213
Access Date2024, May 08
Secondary TypePRE LN
Number of Files1
Size10386 KiB
2. Context
Author1 Jesus, Antonio Delson Conceição de
2 Souza, Marcelo Lopes de Oliveira e
3 Prado, Antonio Fernando Bertchani de Almeida
Group1 DMC-INPE-MCT-BR
EditorWinter, Othon Cabo
Prado, Antonio Fernando Bertachini de Almeida
Book TitleCóloquio Brasileiro de Dinâmica Orbital, 10 Advances in space dynamics 3: applications in astronautics
PublisherINPE
CitySão José dos Campos
Pages363-396
Series TitleAdvances in space dynamics 3: applications in astronautics
History (UTC)2008-06-09 21:41:05 :: administrator -> jefferson ::
2012-08-02 17:55:07 :: jefferson -> administrator ::
2019-01-16 16:15:30 :: administrator -> simone :: 2002
2019-01-16 16:20:01 :: simone -> administrator :: 2002
2021-02-11 18:10:09 :: administrator -> :: 2002
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
KeywordsENGENHARIA E TECNOLOGIA ESPACIAL
manobra orbital
satélite artificial
orbital maneuvers
artificial satellite
AbstractIn this paper we present a survey on the problem of orbital maneuvers for an artificial satellite under different conditions, covering papers starting from 1919. These papers considered several types of orbital maneuvers, including coplanar, non-coplanar, rendezvous, etc. Special orbits are included such as: transfers to the asteroids, aerocaptures, swing-bys, aeroatissisted, etc. Orbits under natural perturbations and transfers under thrust errors are also analyzed. We also considered direct and hybrid solutions to the problem, of orbital maneuvers for an artificial satellite under different conditions without and with errors and/or perturbations. The maneuvers are considered with different constraints (in the semi-major axis, eccentricity, inclination, etc.)with different numbers of propulsion ares. The few papers that study maneuvers with errors are of special interest.
AreaETES
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4. Conditions of access and use
Target FileINPE-9537.pdf
User Groupadministrator
Visibilityshown
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Next Higher Units8JMKD3MGPCW/446AF4B
Host Collectionsid.inpe.br/banon/2001/04.03.15.36
6. Notes
Empty Fieldsaffiliation archivingpolicy archivist callnumber contenttype copyholder copyright creatorhistory descriptionlevel dissemination doi e-mailaddress edition electronicmailaddress isbn issn language lineage mark mirrorrepository nextedition notes numberofvolumes orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup resumeid rightsholder schedulinginformation secondarymark serieseditor session shorttitle sponsor subject tertiarymark tertiarytype translator url versiontype volume


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