1. Identity statement | |
Reference Type | Journal Article |
Site | mtc-m16b.sid.inpe.br |
Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
Identifier | 6qtX3pFwXQZGivnK2Y/ShwPE |
Repository | sid.inpe.br/mtc-m17@80/2007/11.27.17.51 (restricted access) |
Last Update | 2007:11.27.17.54.54 (UTC) administrator |
Metadata Repository | sid.inpe.br/mtc-m17@80/2007/11.27.17.51.20 |
Metadata Last Update | 2021:02.11.18.12.05 (UTC) administrator |
Secondary Key | INPE--PRE/ |
DOI | 10.1016/j.asr.2007.01.012 |
ISSN | 0273-1177 |
Citation Key | Prado:2007:Co‘‘Ap |
Title | A comparison of the ‘‘patched-conics approach’’ and the restricted problem for swing-bys |
Year | 2007 |
Access Date | 2024, Apr. 28 |
Secondary Type | PRE PI |
Number of Files | 1 |
Size | 177 KiB |
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2. Context | |
Author | Prado, Antonio Fernando Bertachini de Almeida |
Resume Identifier | 8JMKD3MGP5W/3C9JGJA |
Group | DMC-INPE-MCT-BR |
Affiliation | Instituto Nacional de Pesquisas Espaciais (INPE) |
Journal | Advances in Space Research |
Volume | 40 |
Number | 1 |
Pages | 113-117 |
History (UTC) | 2007-11-27 18:02:49 :: marciana -> administrator :: 2021-02-11 18:12:05 :: administrator -> marciana :: 2007 |
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3. Content and structure | |
Is the master or a copy? | is the master |
Content Stage | completed |
Transferable | 1 |
Content Type | External Contribution |
Keywords | Astrodynamics Restricted problem Swing-by Space trajectories Jupiter |
Abstract | In the present paper we study swing-by maneuvers that use the planet Jupiter as the body for the close approach. The main goal is to simulate a large variety of initial conditions for those orbits and study the effects caused by the close approach with Jupiter in the orbit of the spacecraft. The planar restricted circular three-body problem and the patched-conics approach are used as the mathematical models. For the planar restricted circular three-body problem, the equations are regularized (using Lemaı tres regularization), so it is possible to avoid the numerical problems that come from the close approach with Jupiter. Then, the results obtained with these well-known dynamics are compared. We see that there is a good agreement of the two models studied in the majority of the situations, but there are large discrepancies in the results of the semi-major axis when the energy before or after the passage is small. There are differences in semi-major axis larger than 10% of the SunJupiter distance in about 5% of the trajectories simulated. Differences in the order of several hundreds of the SunJupiter distances were also encountered. 2007 COSPAR. Published by Elsevier Ltd. All rights reserved. |
Area | ETES |
Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > A comparison of... |
doc Directory Content | access |
source Directory Content | there are no files |
agreement Directory Content | there are no files |
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4. Conditions of access and use | |
Language | en |
Target File | prado4.pdf |
User Group | administrator marciana |
Visibility | shown |
Archiving Policy | denypublisher denyfinaldraft24 |
Read Permission | deny from all and allow from 150.163 |
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5. Allied materials | |
Next Higher Units | 8JMKD3MGPCW/446AF4B |
Dissemination | WEBSCI; PORTALCAPES; MGA; COMPENDEX. |
Host Collection | lcp.inpe.br/ignes/2004/02.12.18.39 cptec.inpe.br/walmeida/2003/04.25.17.12 |
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6. Notes | |
Empty Fields | alternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel documentstage e-mailaddress electronicmailaddress format isbn label lineage mark mirrorrepository month nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup rightsholder schedulinginformation secondarydate secondarymark session shorttitle sponsor subject tertiarymark tertiarytype typeofwork url versiontype |
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7. Description control | |
e-Mail (login) | marciana |
update | |
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