| 1. Identity statement | |
| Reference Type | Journal Article |
| Site | mtc-m16c.sid.inpe.br |
| Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
| Identifier | 8JMKD3MGP8W/35HKSPP |
| Repository | sid.inpe.br/mtc-m18@80/2009/06.26.14.32 (restricted access) |
| Last Update | 2009:06.26.14.32.25 (UTC) administrator |
| Metadata Repository | sid.inpe.br/mtc-m18@80/2009/06.26.14.32.27 |
| Metadata Last Update | 2020:04.28.17.48.42 (UTC) administrator |
| Secondary Key | INPE--PRE/ |
| DOI | 10.1007/s10569-009-9193-6 |
| ISSN | 0923-2958 |
| Citation Key | MeloMacaWint:2009:StPlCh |
| Title | Strategies for plane change of Earth orbits using lunar gravity and derived trajectories of family G  |
| Year | 2009 |
| Month | Apr. |
| Access Date | 2024, May 19 |
| Secondary Type | PRE PI |
| Number of Files | 1 |
| Size | 639 KiB |
| 2. Context | |
| Author | 1 Melo, Cristian Fiorilo 2 Macau, Elbert Einstein Nehrer 3 Winter, O. C. |
| Resume Identifier | 1 2 8JMKD3MGP5W/3C9JGUT |
| Group | 1 LAC-CTE-INPE-MCT-BR 2 LAC-CTE-INPE-MCT-BR |
| Affiliation | 1 Instituto Nacional de Pesquisas Espaciais (INPE) 2 Instituto Nacional de Pesquisas Espaciais (INPE) |
| Journal | Celestial Mechanics and Dynamical Astronomy |
| Volume | 103 |
| Number | 4 |
| Pages | 281-299 |
| History (UTC) | 2009-06-26 14:32:52 :: simone -> administrator :: 2010-05-11 01:08:39 :: administrator -> simone :: 2011-05-20 20:51:55 :: simone -> administrator :: 2020-04-28 17:48:42 :: administrator -> simone :: 2009 |
| 3. Content and structure | |
| Is the master or a copy? | is the master |
| Content Stage | completed |
| Transferable | 1 |
| Content Type | External Contribution |
| Keywords | Astrodynamics Earth-Moon system Mission design Orbital maneuvers Swing-by Gravity assisted maneuver |
| Abstract | The dynamics of the circular restricted three-body Earth-Moon-particle problem predicts the existence of the retrograde periodic orbits around the Lagrangian equilibrium point L1. Such orbits belong to the so-called family G (Broucke, Periodic orbits in the restricted three-body problem with Earth-Moon masses, JPL Technical Report 32-1168, 1968) and starting from them it is possible to define a set of trajectories that form round trip links between the Earth and the Moon. These links occur even with more complex dynamical systems as the complete Sun-Earth-Moon-particle problem. One of the most remarkable properties of these trajectories, observed for the four-body problem, is a meaningful inclination gain when they penetrate into the lunar sphere of influence and accomplish a swing-by with the Moon. This way, when one of these trajectories returns to the proximities of the Earth, it will be in a different orbital plane from its initial Earth orbit. In this work, we present studies that show the possibility of using this property mainly to accomplish transfer maneuvers between two Earth orbits with different altitudes and inclinations, with low cost, taking into account the dynamics of the four-body problem and of the swing-by as well. The results show that it is possible to design a set of nominal transfer trajectories that require Delta V (Total) less than conventional methods like Hohmann, bi-elliptic and bi-parabolic transfer with plane change. |
| Area | COMP |
| Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > LABAC > Strategies for plane... |
| 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 | strategies for plane.pdf |
| User Group | administrator simone |
| Visibility | shown |
| Archiving Policy | denypublisher denyfinaldraft12 |
| Read Permission | deny from all and allow from 150.163 |
| 5. Allied materials | |
| Mirror Repository | sid.inpe.br/mtc-m18@80/2008/03.17.15.17.24 |
| Next Higher Units | 8JMKD3MGPCW/3ESGTTP |
| Dissemination | WEBSCI |
| Host Collection | sid.inpe.br/mtc-m18@80/2008/03.17.15.17 |
| 6. Notes | |
| Empty Fields | alternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel documentstage e-mailaddress electronicmailaddress format isbn label lineage mark nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup rightsholder schedulinginformation secondarydate secondarymark session shorttitle sponsor subject tertiarymark tertiarytype typeofwork url versiontype |
| 7. Description control | |
| e-Mail (login) | simone |
| update | |