<?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/3D53MF8</identifier>
		<repository>dpi.inpe.br/plutao/2012/11.28.16.58</repository>
		<lastupdate>2014:01.15.10.37.46 dpi.inpe.br/plutao@80/2008/08.19.15.01 administrator</lastupdate>
		<metadatarepository>dpi.inpe.br/plutao/2012/11.28.16.58.20</metadatarepository>
		<metadatalastupdate>2021:02.11.18.16.10 sid.inpe.br/bibdigital@80/2006/04.07.15.50 administrator</metadatalastupdate>
		<secondarykey>INPE--PRE/</secondarykey>
		<isbn>21773114</isbn>
		<label>lattes: 3095429508961900 1 SantosRocc:2012:DeFuPi</label>
		<citationkey>SantosRocc:2012:DeFuPi</citationkey>
		<title>Design of a fuzzy pid controller for application in satellite attitude control system</title>
		<format>Papel</format>
		<year>2012</year>
		<secondarytype>PRE CN</secondarytype>
		<numberoffiles>1</numberoffiles>
		<size>1464 KiB</size>
		<author>Santos, Willer Gomes dos,</author>
		<author>Rocco, Evandro Marconi,</author>
		<resumeid></resumeid>
		<resumeid>8JMKD3MGP5W/3C9JH37</resumeid>
		<group></group>
		<group>DMC-ETE-INPE-MCTI-GOV-BR</group>
		<affiliation></affiliation>
		<affiliation>Instituto Nacional de Pesquisas Espaciais (INPE)</affiliation>
		<electronicmailaddress>willer.gomes@yahoo.com.br</electronicmailaddress>
		<e-mailaddress>willer.gomes@yahoo.com.br</e-mailaddress>
		<conferencename>Workshop em Engenharia e Tecnologia Espaciais, 3 (WETE).</conferencename>
		<conferencelocation>São José dos Campos</conferencelocation>
		<date>2012</date>
		<publisher>Instituto Nacional de Pesquisas Espaciais</publisher>
		<volume>3</volume>
		<booktitle>Proceedings</booktitle>
		<tertiarytype>Paper</tertiarytype>
		<transferableflag>1</transferableflag>
		<keywords>controlador PID fuzzy, sistema de controle de atitude, Fuzzy PID controller, attitude control system.</keywords>
		<abstract>In this paper, a fuzzy proportional-integral-derivative (PID) controller is designed to be applied in the satellite attitude control system equipped with reaction wheels. An analysis of the scaling factor is developed to verify its influence during an attitude maneuver. The settling time and the pointing accuracy are the mission requirements that control system have to satisfy. The equations and theoretical concepts are introduced throughout this paper. The results showed that the adequate selection of the scaling factor contributes to the improvement of control results.</abstract>
		<area>ETES</area>
		<language>en</language>
		<targetfile>GomesW_3WETE_2012.pdf</targetfile>
		<usergroup>administrator</usergroup>
		<usergroup>lattes</usergroup>
		<usergroup>marciana</usergroup>
		<readergroup>administrator</readergroup>
		<readergroup>marciana</readergroup>
		<visibility>shown</visibility>
		<readpermission>allow from all</readpermission>
		<documentstage>not transferred</documentstage>
		<nexthigherunit>8JMKD3MGP7W/3E6FERH</nexthigherunit>
		<nexthigherunit>8JMKD3MGPCW/446AF4B</nexthigherunit>
		<citingitemlist>sid.inpe.br/mtc-m19/2013/05.22.14.40 2</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/2012/11.28.16.58</url>
	</metadata>
</metadatalist>