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1. Identity statement
Reference TypeConference Paper (Conference Proceedings)
Sitemarte3.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier6qtX3pFwXQZ3r59YCT/GUQLz
Repositorysid.inpe.br/iris@1905/2005/07.30.02.37   (restricted access)
Last Update2005:09.20.03.00.00 (UTC) administrator
Metadata Repositorysid.inpe.br/iris@1905/2005/07.30.02.37.40
Metadata Last Update2021:02.11.18.23.02 (UTC) administrator
Secondary KeyINPE-9567-PRE/5198
Label10922
Citation KeyLopesCarvSilv:1998:StIdTh
TitleStar Identification for Three-Axis Attitude Estimation of French-Brazilian Scientific Micro-Satellite
Format(paper AAS 98-366)
Year1998
Access Date2024, Apr. 28
Secondary TypePRE PI
Number of Files1
Size269 KiB
2. Context
Author1 Lopes, Roberto Vieira da Fonseca
2 Carvalho, Gustavo B.
3 Silva, Adenilson Roberto
Group1 DMC-INPE-MCT-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
Conference NameAdvances in the Astronautical Sciences.
Volume100
Pages805-819
History (UTC)2005-07-30 02:37:41 :: administrator -> jefferson ::
2005-09-20 16:17:11 :: jefferson -> administrator ::
2012-10-16 03:16:03 :: administrator -> jefferson :: 1998
2013-02-07 17:33:29 :: jefferson -> administrator :: 1998
2021-02-11 18:23:02 :: administrator -> marciana :: 1998
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsENGENHARIA E TECNOLOGIA ESPACIAL
STAR TRACKERS
FLIGHT INSTRUMENTS
SCIENTIFIC SATELLITES
ALGORITHM
SATELLITE ATTITUDE CONTROL
CELESTIAL NAVIGATION
ATTITUDE INDICATORS
STATISTICAL ANALYSIS
SYSTEMS SIMULATION
STELLAR MAGNITUDE
SYSTEMS ANALYSIS
AbstractThis paper investigates full sky star identification methods envisaging their application to attitude determination of the French-Brazilian scientific micro-satellite. A statistical analysis gives a suitable framework to select and adapt an algorithm based on the relationship between star sensor specification and the achievable star identification confidence level under the mission constraints. Attitude determination global performance is presented for a one year long digital simulation, which is intended to give subside to the AOCS design.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Star Identification for...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
Languageen
Target FilePCTEXWIN - AAS98.pdf
User Groupadministrator
jefferson
Visibilityshown
Copy HolderSID/SCD
Archiving Policydenypublisher denyfinaldraft
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Next Higher Units8JMKD3MGPCW/446AF4B
DisseminationWEBSCI; PORTALCAPES; MGA; COMPENDEX.
Host Collectionsid.inpe.br/banon/2001/04.03.15.36
6. Notes
NotesAAS - GSFC International Symposium on Space Flight Dynamics, 13 v.2, p. 775-789.
Empty Fieldsarchivist booktitle callnumber conferencelocation copyright creatorhistory date descriptionlevel doi e-mailaddress edition editor electronicmailaddress isbn issn lineage mark mirrorrepository nextedition numberofvolumes orcid organization parameterlist parentrepositories previousedition previouslowerunit progress project publisher publisheraddress readergroup resumeid rightsholder schedulinginformation secondarydate secondarymark serieseditor session shorttitle sponsor subject tertiarymark tertiarytype type url
7. Description control
e-Mail (login)marciana
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