| 1. Identity statement | |
| Reference Type | Book Section |
| Site | mtc-m16.sid.inpe.br |
| Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
| Repository | sid.inpe.br/marciana/2004/09.13.16.20 |
| Last Update | 2004:09.15.03.00.00 (UTC) administrator |
| Metadata Repository | sid.inpe.br/marciana/2004/09.13.16.20.29 |
| Metadata Last Update | 2021:02.11.18.09.26 (UTC) administrator |
| Secondary Key | INPE-11280-PRE/6717 |
| ISBN/ISSN | 85-17-00012-9 |
| Citation Key | FelipePradBeau:2004:AnDePo |
| Title | An analytical description of the powered swing-by maneuver in three dimensions.  |
| Project | Dinâmica Orbital |
| Year | 2004 |
| Access Date | 2024, Dec. 26 |
| Secondary Type | PRE LI |
| Number of Files | 1 |
| Size | 378 KiB |
| 2. Context | |
| Author | 1 Felipe, Gislaine de 2 Prado, Antonio Fernando Bertachini de Almeida 3 Beaugé, Cristian |
| Resume Identifier | 1 2 8JMKD3MGP5W/3C9JGJA |
| Group | 1 DMC-INPE-MCT-BR |
| Affiliation | 1 Instittuto Nacional de Pesquisas Espaciais. Divisão de Mecânica Espacial e Controle. (INPE.DMC) 2 Universidade Nacional de Cordoba |
| Editor | Kuga, Hélio Koiti |
| e-Mail Address | gislaine@dem.inpe.br |
| Book Title | Advances in space dynamics 4: celestial mechanics and astronautics |
| Publisher | INPE |
| City | São José dos Campos |
| Pages | 15-25 |
| History (UTC) | 2005-07-25 17:01:51 :: jefferson -> administrator :: 2021-02-11 18:09:26 :: administrator -> marciana :: 2004 |
| 3. Content and structure | |
| Is the master or a copy? | is the master |
| Content Stage | completed |
| Transferable | 1 |
| Keywords | SPACE MECHANICS AND CONTROL Orbital dynamics Maneuvers MECÂNICA ESPACIAL E CONTROLE Dinâmica orbital Manobras |
| Abstract | In the present paper we present an analytical description of the powered swing-by maneuver in the three-dimensional space. Analytical equations are derived, based in the patched conics approximation and in the fact that the impulse applied is small compared to the velocity of the spacecraft, in order to calculate the variation in velocity, angular momentum, energy and inclination of the spacecraft during the maneuver. A study is also executed to investigate in which cases the impulse is more efficient when applied during or after the point of maximum approach. Finally, those same maneuvers are computed with the dynamics given by the restricted problem of three bodies and the results are compared with those obtained via the patched-conics approximation. |
| Area | ETES |
| Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > An analytical description... |
| doc Directory Content | access |
| source Directory Content | there are no files |
| agreement Directory Content | there are no files |
| 4. Conditions of access and use | |
| data URL | http://urlib.net/ibi/sid.inpe.br/marciana/2004/09.13.16.20 |
| zipped data URL | http://urlib.net/zip/sid.inpe.br/marciana/2004/09.13.16.20 |
| Language | en |
| Target File | An Analytical.pdf |
| User Group | administrator jefferson |
| Visibility | shown |
| Copy Holder | SID/SCD |
| 5. Allied materials | |
| Next Higher Units | 8JMKD3MGPCW/446AF4B |
| Citing Item List | sid.inpe.br/bibdigital/2021/02.11.18.06 18 sid.inpe.br/mtc-m21/2012/07.13.14.40.20 5 |
| Dissemination | NTRSNASA, BNDEPOSITOLEGAL. |
| Host Collection | sid.inpe.br/banon/2003/08.15.17.40 |
| 6. Notes | |
| Empty Fields | archivingpolicy archivist callnumber contenttype copyright creatorhistory descriptionlevel documentstage doi edition electronicmailaddress format identifier isbn issn label lineage mark mirrorrepository nextedition notes numberofvolumes orcid parameterlist parentrepositories previousedition previouslowerunit progress readergroup readpermission rightsholder schedulinginformation secondarydate secondarymark serieseditor seriestitle session shorttitle sponsor subject tertiarymark tertiarytype translator url versiontype volume |
| 7. Description control | |
| e-Mail (login) | marciana |
| update | |