Combined Quadrotor Autopilot System and Differential Morphing System Design

MakaleAçık Erişim

Özet

The aim of this article is to design and model a quadrotor with autopilot system and differential morphing using the Simultaneous Perturbation Stochastic Approximation (SPSA) optimization algorithm. Along with differential morphing, quadrotor modelling and control was also done. Although it is simple in structure, it has a complex structure in terms of model and control. Newton-Euler method was used for the dynamic model. Non-linear motion equations have been converted to linear motion equations. The full quadrotor model was drawn in the Solidworks program. Mass and moment of inertia information was obtained from this model. Simulation model was created by using state space model approach in Matlab / Simulink environment. Proportional integral derivative (PID) algorithm was used as the control structure. Differential morphing and PID coefficients rates were determined with SPSA. With the optimization method, determining the differential morphing rate, PID coefficients and applying it to the quadrotor provides a very innovative method. 

Anahtar Kelimeler

RDL Kalıcı Bağlantı (PID)
https://rdlopen.rawdatalibrary.net/r/gumushane/17457Resmi atıflarda kullanılan kalıcı adres
DOI
https://doi.org/10.30518/jav.856436Yayıncı resmi DOI adresi
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7
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0
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Tam Kayıt
AlanDeğerDil
dc.contributor.authorOktay, Tugrul
dc.contributor.authorKose, Oguz
dc.date.accessioned2026-10-22T10:38:55.441753023Z
dc.date.available2026-10-22T10:38:55.441753023Z
dc.date.issued2021
dc.description.abstractThe aim of this article is to design and model a quadrotor with autopilot system and differential morphing using the Simultaneous Perturbation Stochastic Approximation (SPSA) optimization algorithm. Along with differential morphing, quadrotor modelling and control was also done. Although it is simple in structure, it has a complex structure in terms of model and control. Newton-Euler method was used for the dynamic model. Non-linear motion equations have been converted to linear motion equations. The full quadrotor model was drawn in the Solidworks program. Mass and moment of inertia information was obtained from this model. Simulation model was created by using state space model approach in Matlab / Simulink environment. Proportional integral derivative (PID) algorithm was used as the control structure. Differential morphing and PID coefficients rates were determined with SPSA. With the optimization method, determining the differential morphing rate, PID coefficients and applying it to the quadrotor provides a very innovative method. 
dc.identifier.doi10.30518/jav.856436
dc.identifier.eissn2587-1676
dc.identifier.endpage71
dc.identifier.issue2
dc.identifier.startpage64
dc.identifier.urihttps://rdlopen.rawdatalibrary.net/r/gumushane/17457
dc.identifier.volume5
dc.language.isoen
dc.relation.ispartofJournal of aviation (Online)
dc.rightsinfo:eu-repo/semantics/openAccess
dc.subjectMühendislik, Elektrik ve Elektronik
dc.subjectBilgisayar Bilimleri, Yazılım Mühendisliği
dc.subjectRobotik
dc.titleCombined Quadrotor Autopilot System and Differential Morphing System Design
dc.typeArticle
rdl.citation.openalex7
rdl.citation.trdizin0
rdl.oa.statusgold
rdl.oa.urlhttps://dergipark.org.tr/en/download/article-file/1496126
rdl.source.indexTRDIZIN