1. Identity statement | |
Reference Type | Journal Article |
Site | mtc-m21b.sid.inpe.br |
Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
Identifier | 8JMKD3MGP3W34P/3Q5932S |
Repository | sid.inpe.br/mtc-m21b/2017/11.30.17.55 (restricted access) |
Last Update | 2017:11.30.17.55.50 (UTC) administrator |
Metadata Repository | sid.inpe.br/mtc-m21b/2017/11.30.17.55.50 |
Metadata Last Update | 2021:02.11.18.12.59 (UTC) administrator |
DOI | 10.1088/1742-6596/911/1/012022 |
ISSN | 1742-6588 |
Citation Key | GonçalvesRoccMora:2017:OrTrDe |
Title | Orbital trajectories in deimos vicinity considering perturbations of gravitational origin |
Year | 2017 |
Access Date | 2024, May 08 |
Type of Work | journal article |
Secondary Type | PRE PI |
Number of Files | 1 |
Size | 985 KiB |
|
2. Context | |
Author | 1 Gonçalves, Liana Dias 2 Rocco, Evandro Marconi 3 Moraes, R. V. de |
Resume Identifier | 1 2 8JMKD3MGP5W/3C9JH37 |
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 Federal de São Paulo (UNIFESP) |
Author e-Mail Address | 1 lianadgon@gmail.com 2 evandro.rocco@inpe.br |
Journal | Journal of Physics: Conference Series |
Volume | 911 |
Pages | 012022 |
Secondary Mark | B2_INTERDISCIPLINAR B2_ENGENHARIAS_III B3_MEDICINA_II B3_GEOCIÊNCIAS B4_MATERIAIS B4_ENGENHARIAS_II B4_BIOTECNOLOGIA C_QUÍMICA C_MATEMÁTICA_/_PROBABILIDADE_E_ESTATÍSTICA C_ENGENHARIAS_IV C_ECONOMIA C_ASTRONOMIA_/_FÍSICA |
History (UTC) | 2017-11-30 17:55:50 :: simone -> administrator :: 2021-02-11 18:12:59 :: administrator -> simone :: 2017 |
|
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 |
Abstract | The present work studies the possibility of maintaining an artificial satellite near to the Deimos surface, even when considering the intense Mars gravitational attraction. For this, a strategy is used in which the spacecraft orbits Mars, but with the same orbital period of Deimos and similar orbital elements. Using this strategy, the deviations in the keplerian elements that characterize the artificial satellite orbit, the magnitude of the main disturbing forces capable of altering the movement of the spacecraft and the variation of the distance between the spacecraft and Deimos are presented. |
Area | ETES |
Arrangement 1 | urlib.net > BDMCI > Fonds > Produção pgr ATUAIS > CMC > Orbital trajectories in... |
Arrangement 2 | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Orbital trajectories in... |
doc Directory Content | access |
source Directory Content | there are no files |
agreement Directory Content | |
|
4. Conditions of access and use | |
Language | en |
Target File | goncalves_orbital.pdf |
User Group | simone |
Visibility | shown |
Archiving Policy | denypublisher denyfinaldraft12 |
Read Permission | deny from all and allow from 150.163 |
Update Permission | not transferred |
|
5. Allied materials | |
Next Higher Units | 8JMKD3MGPCW/3F2UALS 8JMKD3MGPCW/446AF4B |
Dissemination | WEBSCI; PORTALCAPES; SCOPUS. |
Host Collection | sid.inpe.br/mtc-m21b/2013/09.26.14.25.20 |
|
6. Notes | |
Empty Fields | alternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress format isbn keywords label lineage mark mirrorrepository month nextedition notes number 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 | |
|