1. Identity statement | |
Reference Type | Journal Article |
Site | plutao.sid.inpe.br |
Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
Identifier | 8JMKD3MGP3W/3KN2N3N |
Repository | sid.inpe.br/plutao/2015/12.04.12.02.35 (restricted access) |
Last Update | 2015:12.11.12.58.19 (UTC) administrator |
Metadata Repository | sid.inpe.br/plutao/2015/12.04.12.02.36 |
Metadata Last Update | 2021:07.28.22.22.43 (UTC) administrator |
DOI | 10.1088/1742-6596/641/1/012002 |
ISSN | 1742-6588 |
Label | lattes: 7340081273816424 3 FerreiraKugaPradWint:2015:EsTrSp |
Citation Key | FerreiraKugaPradWint:2015:EsTrSp |
Title | Estimating the trajectory of a space vehicle passing by the Moon using Kalman Filter |
Year | 2015 |
Access Date | 2024, June 17 |
Secondary Type | PRE PI |
Number of Files | 1 |
Size | 912 KiB |
|
2. Context | |
Author | 1 Ferreira, A. Ferraz Silva 2 Kuga, Hélio Koiti 3 Prado, Antonio Fernando Bertachini de Almeida 4 Winter, O. C. |
Resume Identifier | 1 2 8JMKD3MGP5W/3C9JHC9 3 8JMKD3MGP5W/3C9JGJA |
Group | 1 2 DMC-ETE-INPE-MCTI-GOV-BR 3 DMC-ETE-INPE-MCTI-GOV-BR |
Affiliation | 1 2 Instituto Nacional de Pesquisas Espaciais (INPE) 3 Instituto Nacional de Pesquisas Espaciais (INPE) 4 Universidade Estadual Paulista (UNESP) |
Author e-Mail Address | 1 aleferrazsilva@hotmail.com 2 helio.kuga@inpe.br 3 antonio.prado@inpe.br |
Journal | Journal of Physics: Conference Series |
Volume | 641 |
Pages | 012002 |
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) | 2015-12-04 12:02:36 :: lattes -> administrator :: 2021-07-28 22:22:43 :: administrator -> simone :: 2015 |
|
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 | Astrodinâmica |
Abstract | The trajectory of a spacecraft going to the periapsis of its orbit around the smaller body of a binary system is estimated from the observed data using a Kalman Filter. Simulations of the trajectories will be made to generate the data of the spacecraft position. When observed from the Earth, using a fixed star as a reference, we have the spacecraft position as an angle function ϕ. This is the angle between spacecraft position vector and the star position vector. The result shows that Kalman Filter can be used successfully for trajectory estimation, if adequate accuracy is available for the angle observations. |
Area | ETES |
Arrangement | urlib.net > DIDMC > Estimating the trajectory... |
doc Directory Content | access |
source Directory Content | there are no files |
agreement Directory Content | there are no files |
|
4. Conditions of access and use | |
Language | pt |
Target File | 1_ferreira3.pdf |
User Group | lattes simone |
Reader Group | administrator simone |
Visibility | shown |
Archiving Policy | denypublisher denyfinaldraft12 |
Read Permission | deny from all and allow from 150.163 |
Update Permission | not transferred |
|
5. Allied materials | |
Mirror Repository | urlib.net/www/2011/03.29.20.55 |
Next Higher Units | 8JMKD3MGPCW/446AF4B |
Citing Item List | sid.inpe.br/bibdigital/2021/02.11.18.06 3 |
Dissemination | WEBSCI; PORTALCAPES; COMPENDEX; SCOPUS. |
Host Collection | dpi.inpe.br/plutao@80/2008/08.19.15.01 |
|
6. Notes | |
Empty Fields | alternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress format isbn lineage mark month nextedition notes number orcid parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject tertiarymark tertiarytype typeofwork url |
|
7. Description control | |
e-Mail (login) | simone |
update | |
|