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		<issn>2236-26-6</issn>
		<citationkey>SouzaSilvOlivLour:2011:SyCoEn</citationkey>
		<title>Systems Concurrent Engineering for the Conception of an attitude and orbit control system</title>
		<format>DVD</format>
		<year>2011</year>
		<secondarytype>PRE CN</secondarytype>
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		<author>Souza, Ariana Cristina Caetano de,</author>
		<author>Silva Neto, Lauro Paulo da,</author>
		<author>Oliva, Leonardo Leite,</author>
		<author>Loureiro, Geilson,</author>
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		<resumeid>8JMKD3MGP5W/3C9JH57</resumeid>
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		<group>LIT-LIT-INPE-MCT-BR</group>
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		<affiliation></affiliation>
		<affiliation></affiliation>
		<affiliation>Instituto Nacional de Pesquisas Espaciais (INPE)</affiliation>
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		<conferencename>Workshop em Engenharia e Tecnologia Espaciais, 2 (WETE).</conferencename>
		<conferencelocation>São José dos Campos</conferencelocation>
		<date>3-4  maio</date>
		<publisher>INPE</publisher>
		<publisheraddress>São José dos Campos</publisheraddress>
		<booktitle>Anais</booktitle>
		<tertiarytype>Sessão Oral</tertiarytype>
		<organization>INPE</organization>
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		<keywords>Engenharia e Gerenciamento em Sistemas Espaciais, Systems concurrent engineering, systems engineering, stakeholders, attitude and orbit control system.</keywords>
		<abstract>This paper presents a systems concurrent engineering approach for the conception of an Attitude and Orbit Control System for a Satellite (AOCS). Systems Engineering uses a multidisciplinary approach in order to better understand complex systems and its processes, its products and its organization. The main goal is to satisfy all stakeholders involved in the product and its processes. In this paper several concepts of Systems Engineering, as well as its methodology, were applied in the main processes of the life cycle of an AOCS of an artificial satellite, in order to give a better understanding of the development of this kind of product, from requirements analysis to system operation.</abstract>
		<area>ETES</area>
		<language>en</language>
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