<?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>Adaptive Nonlinear Controller for Quadrotor Altitude Control with Online Control Coefficients Function</JournalTitle>
			<Issn></Issn>
			<Volume>Volume 17 (2023)</Volume>
			<Issue>Issue 4, December 2023</Issue>
			<PubDate PubStatus="epublish">
                <Year>2024</Year>
                <Month>01</Month>
                <Day>21</Day>
			</PubDate>
		</Journal>
		<ArticleTitle>Adaptive Nonlinear Controller for Quadrotor Altitude Control with Online Control Coefficients Function</ArticleTitle>
		<VernacularTitle></VernacularTitle>
		<FirstPage></FirstPage>
		<LastPage></LastPage>
		<ELocationID EIdType="doi">10.30486/mjee.2023.1986975.1144</ELocationID>
		<Language>EN</Language>
		<AuthorList>
            			<Author>
                				<FirstName>Alireza</FirstName>
				<LastName>Ahangarani Farahani1</LastName>
				<Affiliation>Department of Aerospace Engineering, Malek Ashtar University of Technology, Tehran, Iran</Affiliation>
				<Identifier Source="ORCID"></Identifier>
			</Author>
            			<Author>
                				<FirstName>Sayyed</FirstName>
				<LastName>Majid Hosseini</LastName>
				<Affiliation>Department of Aerospace Engineering, Malek Ashtar University of Technology, Tehran, Iran</Affiliation>
				<Identifier Source="ORCID"></Identifier>
			</Author>
            			<Author>
                				<FirstName>Meysam</FirstName>
				<LastName>Delalat</LastName>
				<Affiliation>Department of Aerospace Engineering, Malek Ashtar University of Technology, Tehran, Iran</Affiliation>
				<Identifier Source="ORCID"></Identifier>
			</Author>
            		</AuthorList>
		<PublicationType>Journal Article</PublicationType>
		<History>
			<PubDate PubStatus="received">
				<Year>2024</Year>
				<Month>01</Month>
				<Day>21</Day>
			</PubDate>
		</History>
		<Abstract>In this paper, an adaptive controller is presented to control a quadrotor, whose parameters are extracted from the genetic algorithm optimization method. The advantage of this method is that based on the system states, the control coefficients are calculated online. For this purpose, a function between system states-space and control coefficients is obtained. From the database collected from the genetic algorithm optimization method, the parameters of the control coefficient function are obtained using the least squares method. The stability of the proposed controller is proved by the Lyapunov method. Finally, the performance of the proposed controller is compared with the PID controller, which is widely used in the literature. The results show that the proposed approach is promising.</Abstract>
		<ObjectList>
            			<Object Type="keyword">
				<Param Name="value">Quadrotor, nonlinear control, Lyapunov Stability, Genetic Algorithm, Gain Tuning. ,</Param>
			</Object>
					</ObjectList>
	</Article>
	</ArticleSet>
