| 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 | Dinâmica Órbital |
| Year | 2006 |
| Month | Apr.-June |
| Access Date | 2024, Apr. 28 |
| Secondary Type | PRE PI |
| Number of Files | 1 |
| Size | 157 KiB |
| 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 |
| 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 Lamaître 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 | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Orbital maneuvers between... |
| doc Directory Content | access |
| source Directory Content | there are no files |
| agreement Directory Content | there are no files |
| 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 |
| 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 |
| 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 |
| 7. Description control | |
| e-Mail (login) | marciana |
| update | |