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1. Identity statement
Reference TypeConference Paper (Conference Proceedings)
Sitemtc-m16d.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP7W/3AQHJ7B
Repositorysid.inpe.br/mtc-m19/2011/11.16.12.15   (restricted access)
Last Update2011:11.16.12.48.46 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m19/2011/11.16.12.15.31
Metadata Last Update2021:02.11.18.18.26 (UTC) administrator
Secondary KeyINPE--PRE/
DOI10.4271/2011-36-0182
Citation KeyTagawaSouz:2011:DiUsIn
TitleA Discussion on the Use of an Integrated Modular Avionics (IMA) Architecture to Simulate an Aerospace Control System
Year2011
Access Date2024, May 05
Secondary TypePRE CI
Number of Files1
Size345 KiB
2. Context
Author1 Tagawa, Gitsuzo de brito Siqueira
2 Souza, Marcelo Lopes de Oliveira e
Resume Identifier1
2 8JMKD3MGP5W/3C9JHP4
Group1
2 DMC-ETE-INPE-MCT-BR
Affiliation1
2 Instituto Nacional de Pesquisas Espaciais (INPE)
Conference NameSAE Brazil Congress - Aerospace, 2011.
Conference LocationSão Paulo
Date4-6 Oct. 2011
VolumeSAE Technical Paper 2011-36-0182
Book TitleProceedings
History (UTC)2012-01-25 12:34:04 :: marciana -> administrator :: 2011
2021-02-11 18:18:26 :: administrator -> marciana :: 2011
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
AbstractThe use of control architectures with the Integrated Modular Avionics (IMA) concept (IMA architectures) in aerospace and the Integrated Modular Electronics (IME) concept (IME architectures) in automotive applications is growing due to its reduced number of hardware such as processors, Line Replaceable Units (LRUs) and Electronic Control Units (ECUs), thereby reducing weight and costs. Furthermore, IMA architectures can perform complex reconfigurations in the case of failures and adapt themselves to changes in network functioning or operating modes, which make a control system very robust. The objective of this work is to discuss the use of an IMA architecture to simulate an aerospace control system responsible for maintaining a vehicle in a predetermined trajectory. To do that, we review the current literature related to IMA architectures and give an overview of their characteristics. Then, we choose an aerospace control system and discuss its simulation using an IMA platform. The preliminary results show: 1) the power and versatility of the IMA architecture used in developing an aerospace control system; 2) the advantages and disadvantages of using Integrated Modular Avionics in aerospace and automotive control systems.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > A Discussion on...
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4. Conditions of access and use
Languageen
Target FileTagawa SAE.pdf
User Groupadministrator
marciana
Visibilityshown
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Mirror Repositorysid.inpe.br/mtc-m19@80/2009/08.21.17.02.53
Next Higher Units8JMKD3MGPCW/446AF4B
Host Collectionsid.inpe.br/mtc-m19@80/2009/08.21.17.02
6. Notes
Empty Fieldsarchivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel dissemination e-mailaddress edition editor electronicmailaddress format isbn issn keywords label lineage mark nextedition notes numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project publisher publisheraddress readergroup rightsholder schedulinginformation secondarydate secondarymark serieseditor session shorttitle sponsor subject tertiarymark tertiarytype type url
7. Description control
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