| 1. Identity statement | ||||
| Reference Type | Journal Article | |||
| Site | mtc-m21c.sid.inpe.br | |||
| Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S | |||
| Identifier | 8JMKD3MGP3W34R/44CK8P8 | |||
| Repository | sid.inpe.br/mtc-m21c/2021/03.22.15.46 | |||
| Last Update | 2021:03.22.15.46.36 (UTC) simone | |||
| Metadata Repository | sid.inpe.br/mtc-m21c/2021/03.22.15.46.36 | |||
| Metadata Last Update | 2022:04.03.19.24.31 (UTC) administrator | |||
| DOI | 10.1007/s40430-021-02914-9 | |||
| ISSN | 1678-5878 | |||
| Citation Key | FerreiraMorPraWinSan:2021:CoApPo | |||
| Title | A computational approach to the powered Swing-By in the elliptic restricted problem  | |||
| Year | 2021 | |||
| Month | Apr. | |||
| Access Date | 2025, July 01 | |||
| Type of Work | journal article | |||
| Secondary Type | PRE PN | |||
| Number of Files | 1 | |||
| Size | 9002 KiB | |||
| 2. Context | ||||
| Author | 1 Ferreira, Alessandra F. S. 2 Moraes, Rodolpho Vilhena 3 Prado, Antonio Fernando Bertachini de Almeida 4 Winter, Othon C. 5 Santtos, Denilson P. S. | |||
| Resume Identifier | 1 2 3 8JMKD3MGP5W/3C9JGJA | |||
| ORCID | 1 0000-0002-6162-9078 2 0000-0003-1289-8332 3 0000-0002-7966-3231 4 0000-0002-4901-3289 5 0000-0003-2682-4043 | |||
| Group | 1 2 3 DIMEC-CGCE-INPE-MCTI-GOV-BR | |||
| Affiliation | 1 Universidade Estadual Paulista (UNESP) 2 Universidade Estadual Paulista (UNESP) 3 Instituto Nacional de Pesquisas Espaciais (INPE) 4 Universidade Estadual Paulista (UNESP) 5 Universidade Estadual Paulista (UNESP) | |||
| Author e-Mail Address | 1 aleferrazsilva@hotmail.com 2 rodolpho.vilhena@gmail.com 3 antonio.prado@inpe.br 4 ocwinter@gmail.com 5 denilson.santos@unesp.br | |||
| Journal | Journal of the Brazilian Society of Mechanical Sciences and Engineering | |||
| Volume | 43 | |||
| Number | 4 | |||
| Pages | e186 | |||
| Secondary Mark | B1_INTERDISCIPLINAR B1_ENGENHARIAS_III B1_ENGENHARIAS_I B1_CIÊNCIAS_AMBIENTAIS B2_MATERIAIS B2_GEOCIÊNCIAS B2_ENGENHARIAS_IV B2_ENGENHARIAS_II B2_ARQUITETURA_E_URBANISMO B3_SAÚDE_COLETIVA B3_ODONTOLOGIA B3_CIÊNCIA_DE_ALIMENTOS B5_MATEMÁTICA_/_PROBABILIDADE_E_ESTATÍSTICA B5_CIÊNCIAS_BIOLÓGICAS_I C_CIÊNCIA_DA_COMPUTAÇÃO C_ASTRONOMIA_/_FÍSICA | |||
| History (UTC) | 2021-03-22 15:46:36 :: simone -> administrator :: 2021-03-22 15:46:37 :: administrator -> simone :: 2021 2021-03-22 15:47:03 :: simone -> administrator :: 2021 2022-04-03 19:24:31 :: administrator -> simone :: 2021 | |||
| 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 · Close approach · Orbital maneuvers · Elliptical system · Energy variation | |||
| Abstract | This work performs a computational investigation of the energy variations given by a powered Swing-By maneuver realized in an elliptical system. It extends previous works by giving the freedom to choose the location and the direction of the thrust vector, aspects that were not considered before in the literature. Those variations are obtained numerically as a function of the parameters related to the thrust (magnitude, direction and location of the application) and the orbital parameters of the primaries (eccentricity and true anomaly). The maneuver is realized around the smaller primary, and the energy variations are measured with respect to the main body of the system. The initial orbit of the space vehicle is defned by its periapsis distance, angle and approach velocity with respect to the smaller primary. The study is applied to a system composed of two primaries that are in elliptic orbits around the center of mass of the system. The eccentricity is varied as a free parameter, to measure its efects. The results show that the best maneuvers apply the thrust at a point inside the sphere of infuence of the secondary body, but not in the periapsis of the orbit. The best direction of the thrust is not aligned with the motion of the space vehicle. The techniques studied here are applied in situations where it is desired to increase the energy of the space vehicle. Empirical equations are obtained for the energy variations, based on the simulations made in the present paper. The numerical approach makes the results more accurate and not limited to particular regions of the eccentricity. | |||
| Area | ETES | |||
| Arrangement | urlib.net > BDMCI > Fonds > Produção a partir de 2021 > CGCE > A computational approach... | |||
| doc Directory Content | access | |||
| source Directory Content | there are no files | |||
| agreement Directory Content |
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| 4. Conditions of access and use | ||||
| data URL | http://urlib.net/ibi/8JMKD3MGP3W34R/44CK8P8 | |||
| zipped data URL | http://urlib.net/zip/8JMKD3MGP3W34R/44CK8P8 | |||
| Language | en | |||
| Target File | ferreira_computational.pdf | |||
| User Group | simone | |||
| Reader Group | administrator simone | |||
| Visibility | shown | |||
| Archiving Policy | allowpublisher allowfinaldraft | |||
| Update Permission | not transferred | |||
| 5. Allied materials | ||||
| Next Higher Units | 8JMKD3MGPCW/46KTFK8 | |||
| Citing Item List | sid.inpe.br/bibdigital/2022/04.03.17.52 - 13 sid.inpe.br/mtc-m21/2012/07.13.14.40.20 - 6 | |||
| Dissemination | WEBSCI; PORTALCAPES. | |||
| Host Collection | urlib.net/www/2017/11.22.19.04 | |||
| 6. Notes | ||||
| Empty Fields | alternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress format isbn label lineage mark mirrorrepository nextedition notes parameterlist parentrepositories previousedition previouslowerunit progress project readpermission rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject tertiarymark tertiarytype url | |||
| 7. Description control | ||||
| e-Mail (login) | simone | |||
| update | ||||