| 1. Identity statement | |
| Reference Type | Journal Article |
| Site | mtc-m16.sid.inpe.br |
| Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
| Identifier | 6qtX3pFwXQZ3r59YDa/JrAqh |
| Repository | sid.inpe.br/iris@1916/2005/12.12.18.25 (restricted access) |
| Last Update | 2013:04.17.17.04.36 (UTC) marciana |
| Metadata Repository | sid.inpe.br/iris@1916/2005/12.12.18.25.41 |
| Metadata Last Update | 2021:02.11.18.10.14 (UTC) administrator |
| Secondary Key | INPE--PRE/ |
| ISSN | 1562-8353 1813-7385 |
| Citation Key | FelipePrad:2005:OpMaUs |
| Title | Optimal maneuvers using a three dimensional gravity assist  |
| Year | 2005 |
| Access Date | 2024, May 01 |
| Secondary Type | PRE PI |
| Number of Files | 1 |
| Size | 133 KiB |
| 2. Context | |
| Author | 1 Felipe, Gislaine de 2 Prado, Antonio Fernando Bertachini de Almeida |
| Group | 1 DMC-INPE-MCT-BR 2 DMC-INPE-MCT-BR |
| Affiliation | 1 Instituto Nacional de Pesquisas Espaciais, Divisão de Mecânica Espacial e Controle (INPE.DMC) 2 Instituto Nacional de Pesquisas Espaciais (INPE) |
| Journal | Nonlinear Dynamics and Systems Theory |
| Volume | 5 |
| Number | 1 |
| Pages | 39-48 |
| History (UTC) | 2006-01-04 11:08:34 :: simone -> administrator :: 2010-05-11 20:13:24 :: administrator -> simone :: 2011-12-19 10:45:25 :: simone -> administrator :: 2005 2013-04-17 16:57:17 :: administrator -> marciana :: 2005 2013-04-17 17:04:37 :: marciana -> administrator :: 2005 2021-02-11 18:10:14 :: administrator -> marciana :: 2005 |
| 3. Content and structure | |
| Is the master or a copy? | is the master |
| Content Stage | completed |
| Transferable | 1 |
| Content Type | External Contribution |
| Version Type | publisher |
| Keywords | Astrodynamics swing-by orbital maneuvers gravity-assist restricted problem |
| Abstract | In the present paper the swing-by maneuvers are studied and classified under the model given by the three-dimensional restricted three-body problem. The modification in the orbit of the spacecraft due to the close approach is shown in plots that specify from which type of orbits the spacecraft is coming and to which type it is going. The results generated here are used to solve optimal problems, such as finding trajectories that satisfy some given constraints (such as achieving an escape or a capture) with some parameters being extremized (position, velocity, etc...). |
| Area | ETES |
| Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Optimal maneuvers using... |
| 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 | 3(10).pdf |
| User Group | administrator marciana simone |
| Visibility | shown |
| Archiving Policy | denypublisher denyfinaldraft |
| Read Permission | deny from all and allow from 150.163 |
| Update Permission | not transferred |
| 5. Allied materials | |
| Next Higher Units | 8JMKD3MGPCW/446AF4B |
| Dissemination | WEBSCI; PORTALCAPES. |
| Host Collection | sid.inpe.br/banon/2003/08.15.17.40 |
| 6. Notes | |
| Empty Fields | alternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel doi e-mailaddress electronicmailaddress format isbn label lineage mark mirrorrepository month nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup resumeid rightsholder schedulinginformation secondarydate secondarymark session shorttitle sponsor subject tertiarymark tertiarytype typeofwork url |
| 7. Description control | |
| e-Mail (login) | marciana |
| update | |