Simultaneous quadrotor autopilot system and collective morphing system design

MakaleYalnız künye

Özet

Purpose: The purpose of this paper is to design a quadrotor with collective morphing using the simultaneous perturbation stochastic approximation (SPSA) optimization algorithm. Design/methodology/approach: Quadrotor design is made by using Solidworks drawing program and some mathematical performance relations. Modelling and simulation are performed in Matlab/Simulink program by using the state space model approaches with the parameters mostly taken from Solidworks. Proportional integral derivative (PID) approach is used as control technique. Morphing amount and the best PID coefficients are determined by using SPSA algorithm. Findings: By using SPSA algorithm, the amount of morphing and the best PID coefficients are determined, and the quadrotor longitudinal and lateral flights are made most stable via morphing. Research limitations/implications: It takes quite a long time to model the quadrotor in Solidworks and Matlab/Simulink with the state space model and using the SPSA algorithm. However, this situation is overcome with the proposed model. Practical implications: Optimization with SPSA is very useful in determining the amount of morphing and PID coefficients for quadrotors. Social implications: SPSA optimization method is useful in terms of cost, time and practicality. Originality/value: It is released to improve performance with morphing, to determine morphing rate with SPSA algorithm and to determine PID coefficients accordingly.

Anahtar Kelimeler

RDL Kalıcı Bağlantı (PID)
https://rdlopen.rawdatalibrary.net/r/gumushane/13015Resmi atıflarda kullanılan kalıcı adres
DOI
https://doi.org/10.1108/aeat-01-2020-0026Yayıncı resmi DOI adresi
Tam Kayıt
AlanDeğerDil
dc.contributor.authorKose, Oguz
dc.contributor.authorOktay, Tugrul
dc.date.accessioned2026-10-22T10:20:49.887305262Z
dc.date.available2026-10-22T10:20:49.887305262Z
dc.date.issued2020
dc.description.abstractPurpose: The purpose of this paper is to design a quadrotor with collective morphing using the simultaneous perturbation stochastic approximation (SPSA) optimization algorithm. Design/methodology/approach: Quadrotor design is made by using Solidworks drawing program and some mathematical performance relations. Modelling and simulation are performed in Matlab/Simulink program by using the state space model approaches with the parameters mostly taken from Solidworks. Proportional integral derivative (PID) approach is used as control technique. Morphing amount and the best PID coefficients are determined by using SPSA algorithm. Findings: By using SPSA algorithm, the amount of morphing and the best PID coefficients are determined, and the quadrotor longitudinal and lateral flights are made most stable via morphing. Research limitations/implications: It takes quite a long time to model the quadrotor in Solidworks and Matlab/Simulink with the state space model and using the SPSA algorithm. However, this situation is overcome with the proposed model. Practical implications: Optimization with SPSA is very useful in determining the amount of morphing and PID coefficients for quadrotors. Social implications: SPSA optimization method is useful in terms of cost, time and practicality. Originality/value: It is released to improve performance with morphing, to determine morphing rate with SPSA algorithm and to determine PID coefficients accordingly.
dc.identifier.doi10.1108/aeat-01-2020-0026
dc.identifier.eissn1758-4213
dc.identifier.endpage1100
dc.identifier.issn1748-8842
dc.identifier.issue7
dc.identifier.scopus2-s2.0-85086256496
dc.identifier.startpage1093
dc.identifier.urihttps://rdlopen.rawdatalibrary.net/r/gumushane/13015
dc.identifier.volume92
dc.identifier.wosWOS:000541533000001
dc.language.isoen
dc.publisherEmerald Publishing
dc.relation.ispartofAircraft Engineering and Aerospace Technology
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.subjectCollective morphing
dc.subjectModelling
dc.subjectOptimization
dc.subjectPID
dc.subjectQuadrotor
dc.subjectSPSA
dc.subjectUAVs
dc.subject.classificationEngineering, Aerospace
dc.subject.classificationEngineering
dc.subject.otherApproximation algorithms
dc.subject.otherOptimization
dc.subject.otherProportional control systems
dc.subject.otherState space methods
dc.subject.otherStochastic systems
dc.subject.otherTwo term control systems
dc.subject.otherApproximation optimization
dc.subject.otherCollective morphing
dc.subject.otherModeling
dc.subject.otherMorphing
dc.subject.otherOptimisations
dc.subject.otherProportional integral derivatives
dc.subject.otherQuad rotors
dc.subject.otherSimultaneous perturbation stochastic approximation
dc.subject.otherSimultaneous perturbation stochastic approximation algorithms
dc.subject.otherSolidWorks
dc.subject.otherSimulink
dc.titleSimultaneous quadrotor autopilot system and collective morphing system design
dc.typeArticle
dspace.entity.typePublication
rdl.citation.openalex70
rdl.citation.scopus67
rdl.citation.wos64
rdl.oa.statusclosed
rdl.source.indexSCOPUS
rdl.source.indexWOS
rdl.wos.indexScience Citation Index Expanded (SCI-EXPANDED)