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1. Identity statement
Reference TypeJournal Article
Sitemarte3.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier6qtX3pFwXQZ3r59YCT/GUPFP
Repositorysid.inpe.br/iris@1905/2005/07.30.01.46   (restricted access)
Last Update2010:03.11.15.09.58 (UTC) administrator
Metadata Repositorysid.inpe.br/iris@1905/2005/07.30.01.46.23
Metadata Last Update2021:02.11.18.13.38 (UTC) administrator
Secondary KeyINPE-9201-PRE/4874
ISSN0100-7386
Label10086
Citation KeyBrumRicc:1994:HoSeAt
TitleHorizon sensors attitude errors simulation for the Brazilian Remote Sensing Satellite
Year1994
Access Date2024, Apr. 28
Secondary TypePRE PN
Number of Files1
Size1893 KiB
2. Context
Author1 Brum, Antonio Gil Vicente de
2 Ricci, Mario Cesar
Group1 DMC-INPE-MCT-BR
2 DMC-INPE-MCT-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
JournalRevista Brasileira de Ciências Mecânicas
Volume16
NumberSpecial Issue
Pages24-23
History (UTC)2008-06-09 16:28:52 :: administrator -> jefferson ::
2010-03-11 15:09:58 :: jefferson -> administrator ::
2021-02-11 18:13:38 :: administrator -> marciana :: 1994
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
KeywordsENGENHARIA E TECNOLOGIA ESPACIAL
ATTITUDE (INCLINATION)
ENVIRONMENTAL RESEARCH SATELLITES
HORIZON SCANNERS
INSTRUMENT ERRORS
PERFORMANCE TESTS
SOFTWARE DEVELOPMENT TOOLS
ACCURACY ATTITUDE STABILITY
BRAZILIAN SPACE PROGRAM
COMPUTERIZED SIMULATION
PERFORMANCE
PREDICTION
AbstractRemote sensing, meteorological and other types of satellites require an increasingly better Earth related positioning. From the past experience it is well known that the thermal horizon in the 15 micrometer band provides conditions of determining the local vertical at any time. This detection is done by horizon sensors which are accurate instruments for Earth referred attitude sensing and control whose performance is limited by systematic and random errors amounting about 0.5 deg. Using the computer programs OBLATE, SEASON, ELECTRO and MISALIGN, developed at INPE to simulate four distinct facets of conical scanning horizon sensors, attitude errors are obtained for the Brazilian Remote Sensing Satellite (the first one, SSR-1, is scheduled to fly in 1996). These errors are due to the oblate shape of the Earth, seasonal and latitudinal variations of the 15 micrometer infrared radiation, electronic processing time delay and misalignment of sensor axis. The sensor related attitude errors are thus properly quantified in this work and will, together with other systematic errors (for instance, ambient temperature variation) take part in the pre-launch analysis of the Brazilian Remote Sensing Satellite, with respect to the horizon sensor performance.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Horizon sensors attitude...
doc Directory Contentaccess
source Directory Contentthere are no files
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4. Conditions of access and use
Target FileDoc2.pdf
User Groupadministrator
jefferson
Visibilityshown
Copy HolderSID/SCD
Archiving Policydenypublisher denyfinaldraft
Read Permissiondeny from all and allow from 150.163
5. Allied materials
Next Higher Units8JMKD3MGPCW/446AF4B
DisseminationPORTALCAPES; SCIELO.
Host Collectionsid.inpe.br/banon/2001/04.03.15.36
6. Notes
NotesInternational Symposium on Spacecraft Ground Control and Flight Dynamics, 7-11 Feb., 1994, São José dos Campos.
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7. Description control
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