| 1. Identity statement | ||||
| Reference Type | Journal Article | |||
| Site | mtc-m21c.sid.inpe.br | |||
| Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S | |||
| Identifier | 8JMKD3MGP3W34R/3SKLFDL | |||
| Repository | sid.inpe.br/mtc-m21c/2019/01.25.14.54 (restricted access) | |||
| Last Update | 2019:01.25.14.54.52 (UTC) administrator | |||
| Metadata Repository | sid.inpe.br/mtc-m21c/2019/01.25.14.54.52 | |||
| Metadata Last Update | 2021:07.28.22.52.25 (UTC) administrator | |||
| DOI | 10.1007/s40314-017-0483-4 | |||
| ISSN | 2238-3603 | |||
| Citation Key | FerreiraPradWint:2018:PlPoSw | |||
| Title | Planar powered Swing-By maneuvers to brake a spacecraft  | |||
| Year | 2018 | |||
| Month | Dec. | |||
| Access Date | 2024, May 08 | |||
| Type of Work | journal article | |||
| Secondary Type | PRE PI | |||
| Number of Files | 1 | |||
| Size | 2726 KiB | |||
| 2. Context | ||||
| Author | 1 Ferreira, Alessandra F. S. 2 Prado, Antonio Fernando Bertachini de Almeida 3 Winter, Othon C. | |||
| Resume Identifier | 1 2 8JMKD3MGP5W/3C9JGJA | |||
| Group | 1 CMC-ETES-SESPG-INPE-MCTIC-GOV-BR 2 DIDMC-CGETE-INPE-MCTIC-GOV-BR | |||
| Affiliation | 1 Instituto Nacional de Pesquisas Espaciais (INPE) 2 Instituto Nacional de Pesquisas Espaciais (INPE) 3 Universidade Estadual Paulista (UNESP) | |||
| Author e-Mail Address | 1 aleferrazsilva@hotmail.com 2 antonio.prado@inpe.br 3 ocwinter@gmail.com | |||
| Journal | Computational and Applied Mathematics | |||
| Volume | 37 | |||
| Number | Suppl. 1 | |||
| Pages | 202-219 | |||
| Secondary Mark | B2_MATEMÁTICA_/_PROBABILIDADE_E_ESTATÍSTICA B2_INTERDISCIPLINAR B3_CIÊNCIA_DA_COMPUTAÇÃO B4_ENGENHARIAS_IV | |||
| History (UTC) | 2019-01-25 14:55:15 :: simone -> administrator :: 2018 2021-07-28 22:52:25 :: administrator -> simone :: 2018 | |||
| 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 | Powered Swing-By Close approach Impulsive maneuvers Spacecraft trajectory Energy decrease | |||
| Abstract | The Swing-By maneuver is a technique used in many space mission to modify the trajectory of a spacecraft. The most usual goal is to increase the energy of the spacecraft, but it is also possible to reduce this energy. An important application is to break a spacecraft coming to the Earth using a Swing-By with the moon, which is the example used in the present paper. Other possibilities also exist, such as reducing the velocity of a spacecraft going to the planets Mercury or Venus. The goal is to help a possible capture by the planet, or at least to provide a passage with smaller velocities to allow better observations during the passage. Therefore, the goal of the present paper is to study the energy loss that a spacecraft may have during a powered Swing-By maneuver, which is a maneuver that combines a close approach by a celestial body with the application of an impulsive maneuver. The behavior of the energy variation is analyzed as a function of the parameters related to the pure gravity maneuver: periapsis radius, angle of approach and approach velocity; and the parameters related to the impulsive maneuver: the location of application of the impulse and its direction and magnitude. The maneuver is performed in a system composed by two bodies, such as the Earth-moon system, around the secondary body, and the energy is measured with respect to the primary body of the system. This problem is solved by developing a mathematical algorithm that guides larger efforts in terms of computer simulations. The results show maps of conditions made from the numerical simulations for different points of application and direction of the impulse, where the maneuver is advantageous and how much more energy can be removed from the spacecraft. | |||
| Area | ETES | |||
| Arrangement 1 | urlib.net > BDMCI > Fonds > Produção pgr ATUAIS > CMC > Planar powered Swing-By... | |||
| Arrangement 2 | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Planar powered Swing-By... | |||
| doc Directory Content | access | |||
| source Directory Content | there are no files | |||
| agreement Directory Content |
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| 4. Conditions of access and use | ||||
| Language | en | |||
| Target File | ferreira_planar.pdf | |||
| User Group | simone | |||
| Visibility | shown | |||
| Read Permission | deny from all and allow from 150.163 | |||
| Update Permission | not transferred | |||
| 5. Allied materials | ||||
| Mirror Repository | urlib.net/www/2017/11.22.19.04.03 | |||
| Next Higher Units | 8JMKD3MGPCW/3F2UALS 8JMKD3MGPCW/446AF4B | |||
| Dissemination | WEBSCI; PORTALCAPES; SCOPUS. | |||
| Host Collection | urlib.net/www/2017/11.22.19.04 | |||
| 6. Notes | ||||
| Empty Fields | alternatejournal archivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress format isbn label lineage mark nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject tertiarymark tertiarytype url | |||
| 7. Description control | ||||
| e-Mail (login) | simone | |||
| update | ||||