<?xml version="1.0" encoding="ISO-8859-1"?>
<metadatalist>
	<metadata ReferenceType="Conference Proceedings">
		<site>plutao.sid.inpe.br 800</site>
		<holdercode>{isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S}</holdercode>
		<identifier>J8LNKAN8RW/39RQ9JC</identifier>
		<repository>dpi.inpe.br/plutao/2011/06.11.02.35.52</repository>
		<lastupdate>2012:04.18.11.41.32 dpi.inpe.br/plutao@80/2008/08.19.15.01 marciana</lastupdate>
		<metadatarepository>dpi.inpe.br/plutao/2011/06.11.02.35.53</metadatarepository>
		<metadatalastupdate>2021:02.11.20.56.43 sid.inpe.br/bibdigital@80/2006/04.07.15.50 administrator</metadatalastupdate>
		<secondarykey>INPE--PRE/</secondarykey>
		<issn>2236-2606</issn>
		<label>lattes: 3237709114127674 1 RomeroFerr:2011:MOATOR</label>
		<citationkey>RomeroFerr:2011:MoAtOr</citationkey>
		<title>Modeling an attitude and orbit control system using sysml</title>
		<format>DVD</format>
		<year>2011</year>
		<secondarytype>PRE CN</secondarytype>
		<numberoffiles>1</numberoffiles>
		<size>412 KiB</size>
		<author>Romero, Alessandro Gerlinger,</author>
		<author>Ferreira, Mauricio Gonçalves Vieira,</author>
		<group>DSE-ETE-INPE-MCT-BR</group>
		<group>CRC-CRC-INPE-MCT-BR</group>
		<affiliation>Instituto Nacional de Pesquisas Espaciais (INPE)</affiliation>
		<affiliation>Instituto Nacional de Pesquisas Espaciais (INPE)</affiliation>
		<electronicmailaddress>romgerale@hotmail.com</electronicmailaddress>
		<electronicmailaddress></electronicmailaddress>
		<e-mailaddress>romgerale@hotmail.com</e-mailaddress>
		<conferencename>Workshop em Engenharia e Tecnologia Espaciais, 2 (WETE).</conferencename>
		<conferencelocation>Sao Jose dos Campos</conferencelocation>
		<date>3-4  maio</date>
		<publisher>INPE</publisher>
		<publisheraddress>São José dos Campos</publisheraddress>
		<booktitle>Anais</booktitle>
		<organization>INPE</organization>
		<transferableflag>1</transferableflag>
		<keywords>Engenharia e Gerenciamento em Sistemas Espaciais, SysML, system engineering, MDA, PIM, PSM, code generation.</keywords>
		<abstract>This paper presents an approach for development process of an Attitude and Orbit Control System (AOCS) software for a satellite using SysML (Systems Modeling Language). The development process starts analyzing context diagram, stakeholder and their needs. So it is derived system requirements and measure of effectiveness (MoEs). After this a functional analysis is accomplished using use cases. Constraints and parametric diagrams are described. Physical aspects are modeled and considered to model behavior using sequence diagrams. Finally, model is refined to become a PSM model from software viewpoint, allowing code generation.</abstract>
		<area>ETES</area>
		<language>pt</language>
		<targetfile>1002-4.pdf</targetfile>
		<usergroup>lattes marciana</usergroup>
		<visibility>shown</visibility>
		<readpermission>allow from all</readpermission>
		<documentstage>not transferred</documentstage>
		<nexthigherunit>8JMKD3MGP7W/3E9SLB5</nexthigherunit>
		<nexthigherunit>8JMKD3MGPCW/3F3PAJE</nexthigherunit>
		<nexthigherunit>8JMKD3MGPCW/446AUSL</nexthigherunit>
		<citingitemlist>sid.inpe.br/mtc-m19/2013/06.12.14.47 4</citingitemlist>
		<citingitemlist>sid.inpe.br/bibdigital/2013/10.19.00.29 2</citingitemlist>
		<citingitemlist>sid.inpe.br/bibdigital/2021/02.11.20.54 1</citingitemlist>
		<hostcollection>dpi.inpe.br/plutao@80/2008/08.19.15.01</hostcollection>
		<username>marciana</username>
		<lasthostcollection>dpi.inpe.br/plutao@80/2008/08.19.15.01</lasthostcollection>
		<url>http://plutao.sid.inpe.br/rep-/dpi.inpe.br/plutao/2011/06.11.02.35.52</url>
	</metadata>
</metadatalist>