| 1. Identity statement | |
| Reference Type | Conference Paper (Conference Proceedings) |
| Site | mtc-m21c.sid.inpe.br |
| Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
| Identifier | 8JMKD3MGP3W34R/3U9HMN8 |
| Repository | sid.inpe.br/mtc-m21c/2019/10.22.15.10 |
| Last Update | 2019:10.22.15.10.12 (UTC) simone |
| Metadata Repository | sid.inpe.br/mtc-m21c/2019/10.22.15.10.12 |
| Metadata Last Update | 2020:01.06.11.42.23 (UTC) administrator |
| Secondary Key | INPE--PRE/ |
| Citation Key | Macau:2019:FoDyEx |
| Title | Building inclinated and excentric high earth orbits through small perturbations: a four-body dynamics exploration  |
| Year | 2019 |
| Access Date | 2024, May 19 |
| Secondary Type | PRE CI |
| Number of Files | 1 |
| Size | 34 KiB |
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| 2. Context | |
| Author | Macau, Elbert Einstein Nehrer |
| Resume Identifier | 8JMKD3MGP5W/3C9JGUT |
| Group | LABAC-COCTE-INPE-MCTIC-GOV-BR |
| Affiliation | Instituto Nacional de Pesquisas Espaciais (INPE) |
| Author e-Mail Address | elbert.macau@inpe.br |
| Conference Name | International Astronautical Congress, 70.; IAF Astrodynamics Symposium |
| Conference Location | Washington, DC |
| Date | 21-25 Oct. |
| History (UTC) | 2019-10-22 15:10:12 :: simone -> administrator ::
2020-01-06 11:42:23 :: administrator -> simone :: 2019 |
|
| 3. Content and structure | |
| Is the master or a copy? | is the master |
| Content Stage | completed |
| Transferable | 1 |
| Content Type | External Contribution |
| Abstract | In specific applications, such as communication missions, require orbits with large journey time between the apogee and perigee, thus remaining for long periods at a specific point in space. Normally in these cases, the final inclination, eccentricity and semimajor axis values aimed demand too much fuel consumption when conducted by the conventional transfers methods. In this work, an alternative strategy transfer is proposed. It consists of exploring and take advantage of the natural dynamics associated to the unstable orbits and sensitive dependence present in the four body problem. In this perspective, a low cost transfer starting from a low to a high and inclinated Earth orbit is built through a combination of a lunar gravity assisted maneuver and the application of judicious and small impulses to specific points of the trajectory. The method was validated in case studies carried out for a scenario composed of Sun, Earth, Moon and vehicle. The results obtained show that it is possible to obtain the desired stable orbits with a low total impulse magnitude, even in cases where conventional transfer methods are not feasible. |
| Area | COMP |
| Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > LABAC > Building inclinated and... |
| 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://mtc-m21c.sid.inpe.br/ibi/8JMKD3MGP3W34R/3U9HMN8 |
| zipped data URL | http://mtc-m21c.sid.inpe.br/zip/8JMKD3MGP3W34R/3U9HMN8 |
| Language | en |
| Target File | macau_building.pdf |
| User Group | simone |
| Visibility | shown |
| Update Permission | not transferred |
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| 5. Allied materials | |
| Next Higher Units | 8JMKD3MGPCW/3ESGTTP |
| Citing Item List | sid.inpe.br/mtc-m21/2012/07.13.14.45.07 1 |
| Host Collection | urlib.net/www/2017/11.22.19.04 |
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| 6. Notes | |
| Empty Fields | archivingpolicy archivist booktitle callnumber copyholder copyright creatorhistory descriptionlevel dissemination doi e-mailaddress edition editor format isbn issn keywords label lineage mark mirrorrepository nextedition notes numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project publisher publisheraddress readergroup readpermission rightsholder schedulinginformation secondarydate secondarymark serieseditor session shorttitle sponsor subject tertiarymark tertiarytype type url versiontype volume |
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| 7. Description control | |
| e-Mail (login) | simone |
| update | |
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