1. Identity statement | |
Reference Type | Journal Article |
Site | mtc-m16b.sid.inpe.br |
Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
Identifier | 6qtX3pFwXQZGivnK2Y/Shwqd |
Repository | sid.inpe.br/mtc-m17@80/2007/11.27.17.30.15 (restricted access) |
Last Update | 2007:11.27.17.46.35 (UTC) administrator |
Metadata Repository | sid.inpe.br/mtc-m17@80/2007/11.27.17.30.16 |
Metadata Last Update | 2021:02.11.18.12.05 (UTC) administrator |
Secondary Key | INPE--PRE/ |
DOI | 10.1016/j.asr.2007.04.098 |
ISSN | 0273-1177 |
Citation Key | PradoFeli:2007:AnStPo |
Title | An analytical study of the powered swing-by to perform orbital maneuvers |
Year | 2007 |
Access Date | 2024, Apr. 28 |
Secondary Type | PRE PI |
Number of Files | 1 |
Size | 591 KiB |
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2. Context | |
Author | 1 Prado, Antonio Fernando Bertachini de Almeida 2 Felipe, Gislaine de |
Resume Identifier | 1 8JMKD3MGP5W/3C9JGJA |
Group | 1 DMC-INPE-MCT-BR 2 DMC-INPE-MCT-BR |
Affiliation | 1 Instituto Nacional de Pesquisas Espaciais (INPE) 2 Instituto Nacional de Pesquisas Espaciais (INPE) |
Journal | Advances in Space Research |
Volume | 40 |
Number | 12 |
Pages | 1769-1968 |
History (UTC) | 2007-11-27 18:03:27 :: marciana -> administrator :: 2010-05-11 02:11:49 :: administrator -> marciana :: 2011-05-20 22:30:43 :: 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 Swing-by Orbital maneuvers Patched-conics approximation |
Abstract | In the present paper, we present an analytical description of the powered swing-by maneuver in the three-dimensional space. To perform this task, new analytical equations are derived for the three-dimensional unpowered swing-by, including the variation in velocity, angular momentum, energy and inclination of the spacecraft due to the maneuver. This is done based on the patched-conics approximation. From those general three-dimensional equations, it is possible to confirm some well-known analytical results for the planar case. The equations developed here are verified by numerical integrations, using the restricted problem of three bodies, showing an agreement better than 1%. After that, based on those equations, some new analytical results are obtained for the situation when an impulse is applied to the spacecraft during the close approach. Those new equations are based in the assumption that the impulse applied is small compared to the velocity of the spacecraft, and they allow the calculation of the same variations cited above. Those equations can be simplified for specific cases, and it can generate some conclusions about the direction to apply the impulse to attend specific goals. A study is also executed to investigate in which cases the impulse is more efficient when applied at the periapsis of the swing-by hyperbola or at points far way from the swing-by body. |
Area | ETES |
Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > An analytical study... |
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 | prado3.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 |
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