1. Identity statement | |
Reference Type | Journal Article |
Site | mtc-m16b.sid.inpe.br |
Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
Identifier | 6qtX3pFwXQZGivnK2Y/NqHev |
Repository | sid.inpe.br/mtc-m17@80/2006/12.11.13.34 (restricted access) |
Last Update | 2006:12.11.13.34.42 (UTC) administrator |
Metadata Repository | sid.inpe.br/mtc-m17@80/2006/12.11.13.34.43 |
Metadata Last Update | 2021:02.11.18.11.47 (UTC) administrator |
Secondary Key | INPE-14437-PRE/9517 |
ISSN | 0100-7386 |
Citation Key | Prado:2006:OrMaTh |
Title | Orbital maneuvers between the lagrangian points and the primaries in the Earth-Sun system |
Project | Dināmica Órbital |
Year | 2006 |
Month | Apr.-June |
Access Date | 2024, May 13 |
Secondary Type | PRE PI |
Number of Files | 1 |
Size | 157 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) |
Author e-Mail Address | prado@dem.inpe.br |
Journal | Journal of the Brazilian Society of Mechanical Sciences and Engineering |
Volume | 28 |
Number | 2 |
Pages | 131-139 |
History (UTC) | 2007-03-20 12:53:56 :: vinicius -> administrator :: 2008-06-29 02:30:00 :: administrator -> vinicius :: 2011-05-29 09:26:43 :: vinicius -> administrator :: 2012-11-24 01:39:44 :: administrator -> vinicius :: 2006 2013-02-20 16:29:36 :: vinicius -> administrator :: 2006 2021-02-11 18:11:47 :: administrator -> marciana :: 2006 |
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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 | ENGENHARIA E TECNOLOGIA ESPACIAIS astrodynamics lagrangian points orbital maneuvers impulsive transfers |
Abstract | This paper is concerned with trajectories to transfer a spacecraft between the Lagrangian points of the Sun-Earth system and the primaries. The Lagrangian points have important applications in astronautics, since they are equilibrium points of the equation of motion and very good candidates to locate a satellite or a space station. The planar circular restricted three-body problem in two dimensions is used as the model for the Sun-Earth system, and Lamaītre regularization is used to avoid singularities during the numerical integration required to solve the Lambert's three-body problem. The results show families of transfer orbits, parameterized by the transfer time. |
Area | ETES |
Arrangement | Orbital maneuvers between... |
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 | prado-orbital maneuvers.pdf |
User Group | administrator vinicius |
Visibility | shown |
Copy Holder | SID/SCD |
Archiving Policy | denypublisher denyfinaldraft |
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. |
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 copyright creatorhistory descriptionlevel documentstage doi e-mailaddress format isbn label lineage mark mirrorrepository nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress 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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