<?xml version="1.0" encoding="UTF-8"?><!DOCTYPE ArticleSet PUBLIC "-//NLM//DTD PubMed 2.7//EN" "https://dtd.nlm.nih.gov/ncbi/pubmed/in/PubMed.dtd">
<ArticleSet>
		<Article>
		<Journal>
			<PublisherName>Majlesi Journal of Electrical Engineering</PublisherName>
			<JournalTitle>Design of Integral Augmented Sliding Mode Control for Pitch Angle of a 3-DOF Bench-top Helicopter</JournalTitle>
			<Issn></Issn>
			<Volume>Volume 4 (2010)</Volume>
			<Issue>Issue 3, September 2010</Issue>
			<PubDate PubStatus="epublish">
                <Year>2024</Year>
                <Month>02</Month>
                <Day>26</Day>
			</PubDate>
		</Journal>
		<ArticleTitle>Design of Integral Augmented Sliding Mode Control for Pitch Angle of a 3-DOF Bench-top Helicopter</ArticleTitle>
		<VernacularTitle></VernacularTitle>
		<FirstPage></FirstPage>
		<LastPage></LastPage>
		<ELocationID EIdType="doi">10.1234/mjee.v4i3.338</ELocationID>
		<Language>EN</Language>
		<AuthorList>
            			<Author>
                				<FirstName>Amir</FirstName>
				<LastName>Zaeri</LastName>
				<Affiliation>UPM</Affiliation>
				<Identifier Source="ORCID"></Identifier>
			</Author>
            			<Author>
                				<FirstName>Samsul</FirstName>
				<LastName>Bahari Mohd Noor</LastName>
				<Affiliation></Affiliation>
				<Identifier Source="ORCID"></Identifier>
			</Author>
            			<Author>
                				<FirstName>Maryam</FirstName>
				<LastName>Mohd Isa</LastName>
				<Affiliation></Affiliation>
				<Identifier Source="ORCID"></Identifier>
			</Author>
            			<Author>
                				<FirstName>Farah</FirstName>
				<LastName>Saleena Taip</LastName>
				<Affiliation></Affiliation>
				<Identifier Source="ORCID"></Identifier>
			</Author>
            		</AuthorList>
		<PublicationType>Journal Article</PublicationType>
		<History>
			<PubDate PubStatus="received">
				<Year>2024</Year>
				<Month>02</Month>
				<Day>26</Day>
			</PubDate>
		</History>
		<Abstract>Sliding mode control (SMC) is a nonlinear controller that is used to achieve desired performance in the presence of unstructured uncertainty as a result of carelessness of parameter specification of the system. The main aim for sliding control, or also called Variable Structure Control, is to control the nonlinear plant by introducing a sliding surface. The sliding surface should be reached by making the state of system approach this level. In this paper, an integral augmented sliding mode control (SMC+I) is proposed to improve the control performance of a plant with uncertainty giving the example of bench-top helicopter and the results are compared with the results obtained from conventional sliding mode control with and without a boundary layer.   </Abstract>
		<ObjectList>
            			<Object Type="keyword">
				<Param Name="value">chattering phenomenon</Param>
			</Object>
						<Object Type="keyword">
				<Param Name="value">Boundary layer</Param>
			</Object>
						<Object Type="keyword">
				<Param Name="value">Pitch Angel of a 3-DOF Helicopter.</Param>
			</Object>
						<Object Type="keyword">
				<Param Name="value">sliding mode control</Param>
			</Object>
					</ObjectList>
	</Article>
	</ArticleSet>
