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		<identifier>8JMKD3MGP3W/3RANGUJ</identifier>
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		<doi>10.1007/978-3-319-65283-2_31</doi>
		<isbn>9783319652825</isbn>
		<label>lattes: 2129756520636332 2 LeiteFoGuimGale:2018:MIAtCo</label>
		<citationkey>LeiteFoGuimGale:2018:MIAtCo</citationkey>
		<title>MIMO attitude control for a spinning rocket</title>
		<year>2018</year>
		<secondarytype>PRE LI</secondarytype>
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		<size>2914 KiB</size>
		<author>Leite Filho, Waldemar de Castro,</author>
		<author>Guimarães, Júlia de Albuquerque,</author>
		<author>Galembeck, Lucas,</author>
		<group>CMC-ETES-SESPG-INPE-MCTIC-GOV-BR</group>
		<group>CMC-ETES-SESPG-INPE-MCTIC-GOV-BR</group>
		<affiliation>Instituto Nacional de Pesquisas Espaciais (INPE)</affiliation>
		<affiliation>Instituto Nacional de Pesquisas Espaciais (INPE)</affiliation>
		<affiliation>Instituto Nacional de Pesquisas Espaciais (INPE)</affiliation>
		<electronicmailaddress>waldclf@gmail.com</electronicmailaddress>
		<editor>Dolega, Buguslaw,</editor>
		<editor>Glebocki, Robert,</editor>
		<editor>Kordos, Damian,</editor>
		<editor>Zugaj, Marcin,</editor>
		<booktitle>Advances in aerospace guidance, navigation and control</booktitle>
		<publisher>Springer International Publishing</publisher>
		<pages>571-584</pages>
		<transferableflag>1</transferableflag>
		<contenttype>External Contribution</contenttype>
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		<keywords>MIMO, attitude control.</keywords>
		<abstract>When dealing with rockets that present no direct roll control, it is possible that disturbances along the system may introduce some roll rate [10]. The highly coupled nature of the rockets equations of motion make the study of its dynamic a very complex subject [7, 9]. It is necessary to understand how well a given control system is able to deal with such perturbations. In this paper, we are interested in studying the performance of a multiple-inputmultiple-output (MIMO) controller with roll input and how it compares to a singleinput-single-output (SISO) PID controller when used on a rocket under the influence of an uncontrolled spin rate of parabolic profile. The controllers are compared by analyzing both step response and the ability to send the system to a pre-determined trajectory, with and without the influence of wind perturbations.</abstract>
		<area>ETES</area>
		<language>pt</language>
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		<url>http://link.springer.com/10.1007/978-3-319-65283-2_31</url>
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