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dc.contributor.authorCan, Muharrem Selim
dc.contributor.authorErcan, Hamdi
dc.date.accessioned2021-12-29T10:45:58Z
dc.date.available2021-12-29T10:45:58Z
dc.date.issued2021en_US
dc.identifier.citationCan, M.S., Ercan, H. (2021). Real-time tuning of PID controller based on optimization algorithms for a quadrotor. Aircraft Engineering and Aerospace Technology. https://doi.org/10.1108/AEAT-06-2021-0173en_US
dc.identifier.urihttps://doi.org/10.1108/AEAT-06-2021-0173
dc.identifier.urihttps://hdl.handle.net/20.500.12508/2018
dc.description.abstractPurpose This study aims to develop a quadrotor with a robust control system against weight variations. A Proportional-Integral-Derivative (PID) controller based on Particle Swarm Optimization and Differential Evaluation to tune the parameters of PID has been implemented with real-time simulations of the quadrotor. Design/methodology/approach The optimization algorithms are combined with the PID control mechanism of the quadrotor to increase the performance of the trajectory tracking for a quadrotor. The dynamical model of the quadrotor is derived by using Newton-Euler equations. Findings In this study, the most efficient control parameters of the quadrotor are selected using evolutionary optimization algorithms in real-time simulations. The control parameters of PID directly affect the controller's performance that position error and stability improved by tuning the parameters. Therefore, the optimization algorithms can be used to improve the trajectory tracking performance of the quadrotor. Practical implications The online optimization result showed that evolutionary algorithms improve the performance of the trajectory tracking of the quadrotor. Originality/value This study states the design of an optimized controller compared with manually tuned controller methods. Fitness functions are defined as a custom fitness function (overshoot, rise-time, settling-time and steady-state error), mean-square-error, root-mean-square-error and sum-square-error. In addition, all the simulations are performed based on a realistic simulation environment. Furthermore, the optimization process of the parameters is implemented in real-time that the proposed controller searches better parameters with real-time simulations and finds the optimal parameter online.en_US
dc.language.isoengen_US
dc.publisherEmerald Group Publishing Ltd.en_US
dc.relation.isversionof10.1108/AEAT-06-2021-0173en_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectNonlinear controlen_US
dc.subjectNumerical optimization algorithmsen_US
dc.subjectProportional-integral-derivative (PID) controlen_US
dc.subjectQuadrotor dynamicsen_US
dc.subjectReal-time simulationsen_US
dc.subject.classificationEngineering
dc.subject.classificationTrajectory Tracking
dc.subject.classificationAltitude Control
dc.subject.classificationVertical Takeoff and Landing
dc.subject.otherDifferential evolution
dc.subject.otherGenetic algorithm
dc.subject.otherFlight control
dc.subject.otherParameters
dc.subject.otherControllers
dc.subject.otherErrors
dc.subject.otherMean square error
dc.subject.otherParameter estimation
dc.subject.otherParticle swarm optimization (PSO)
dc.subject.otherRobust control
dc.subject.otherThree term control systems
dc.subject.otherTrajectories
dc.subject.otherTwo term control systems
dc.titleReal-time tuning of PID controller based on optimization algorithms for a quadrotoren_US
dc.typearticleen_US
dc.relation.journalAircraft Engineering and Aerospace Technologyen_US
dc.contributor.departmentHavacılık ve Uzay Bilimleri Fakültesi -- Havacılık Elektrik ve Elektroniği Bölümüen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.contributor.isteauthorCan, Muharrem Selim
dc.relation.indexWeb of Science - Scopusen_US
dc.relation.indexWeb of Science Core Collection - Science Citation Index Expanded


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