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Enhancing performance and stability of gain-scheduling control system using evolutionary algorithms: A case study on transport aircraft

dc.contributor.authorElkhatem, Aisha Sir
dc.contributor.authorEngin, Seref Naci
dc.date.accessioned2026-06-27T14:39:50Z
dc.date.issued2023
dc.description.abstractAn enhanced gain-scheduling control strategy was presented to establish a smooth adaptation mechanism for the longitudinal motion of B747 between different flight envelopes. The focal objective is to accomplish a smooth and non-conservative gain-scheduling control system that has high performance and stability characteristics for different flight conditions and transitions between them. The proposed approach ensured a successful gain scheduling control system by allocating a specific error performance index that should be minimized for all flight conditions. Then all required performance indices were cohered according to the flight envelope in the form of a multi-objective optimization problem that could be solved using evolutionary algorithms. The performance and stability of the transition points between different flight conditions were preserved through the sets of feasible solutions obtained by an evolutionary algorithm which are known as a set of Pareto optimal solutions. The proposed gain-scheduling system was built based on 2DoF-PID (Two-degree-of-freedom Proportional Integral Derivative) controller. An auto-decision-maker was developed to adjust the parameters of the 2DoF-PID gainscheduling control system with the current flight condition. The effectiveness of the proposed gain-scheduling control structure was studied for two different multiobjective evolutionary-based optimizers known as fast sorting and elite multi-objective genetic algorithm.II (NSGA.II), and sub-population genetic algorithm.II (SPGA. II). The proposed methodology was evaluated by simulation results according to the quality of the pareto-front and transient response characteristics of the proposed gain-scheduling controller for the chosen flight conditions in normal flight conditions and 50% loss of actuator effectiveness.en
dc.description.urihttps://doi.org/10.1016/j.eswa.2022.118859
dc.identifier.doi10.1016/j.eswa.2022.118859
dc.identifier.eissn1873-6793
dc.identifier.issn0957-4174
dc.identifier.urihttps://hdl.handle.net/20.500.14981/63251
dc.identifier.volume213
dc.identifier.wos000870841400002
dc.language.isoeng
dc.publisherPERGAMON-ELSEVIER SCIENCE LTD
dc.relation.ispartofEXPERT SYSTEMS WITH APPLICATIONS
dc.subjectSmooth adaptation mechanism
dc.subjectGain scheduling flight control
dc.subjectEvolutionary algorithms
dc.subjectNon -dominated optimal solutions
dc.subjectLongitudinal motion of B747
dc.subjectTAKAGI-SUGENO
dc.subjectLPV CONTROL
dc.subjectIDENTIFICATION
dc.subjectOPTIMIZATION
dc.subjectComputer Science
dc.subjectEngineering
dc.subjectOperations Research & Management Science
dc.titleEnhancing performance and stability of gain-scheduling control system using evolutionary algorithms: A case study on transport aircraft
dc.typeArticle
dspace.entity.typePublication
local.import.sourceWOS

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