Octorotor flight control system design with stochastic optimal tuning, deep learning and differential morphing

ArticleAçık Erişim

Özet

In this paper, simultaneous longitudinal and lateral flight control is investigated for an octorotor by using stochastic optimal tuning and deep learning under differential morphing. Octorotor models for differential morphing were drawn in SOLIDWORKS drawing program. Arm lengths are randomly estimated in the algorithm. Moments of inertia changing according to morphing ratios are estimated with deep neural network. In addition, the proportional–integral–derivative controller coefficients required for both longitudinal and lateral flight according to the morphing ratios are estimated by simultaneous perturbation stochastic approximation. Considering the design performance criteria, 49.95% improvement was achieved in the total cost. The estimation of unknown parameters by optimization method and deep learning was tested in simulations, and the octorotor successfully followed the given reference angle. © The Author(s), under exclusive licence to The Brazilian Society of Mechanical Sciences and Engineering 2024.

Anahtar Kelimeler

RDL Kalıcı Bağlantı (PID)
https://rdlopen.rawdatalibrary.net/r/ebyu/11885Resmi atıflarda kullanılan kalıcı adres
DOI
https://doi.org/10.1007/s40430-024-04972-1Yayıncı resmi DOI adresi
Tam Kayıt
AlanDeğerDil
dc.contributor.authorKose, Oguz
dc.date.accessioned2026-10-18T20:26:52.446617691Z
dc.date.available2026-10-18T20:26:52.446617691Z
dc.date.issued2024
dc.description.abstractIn this paper, simultaneous longitudinal and lateral flight control is investigated for an octorotor by using stochastic optimal tuning and deep learning under differential morphing. Octorotor models for differential morphing were drawn in SOLIDWORKS drawing program. Arm lengths are randomly estimated in the algorithm. Moments of inertia changing according to morphing ratios are estimated with deep neural network. In addition, the proportional–integral–derivative controller coefficients required for both longitudinal and lateral flight according to the morphing ratios are estimated by simultaneous perturbation stochastic approximation. Considering the design performance criteria, 49.95% improvement was achieved in the total cost. The estimation of unknown parameters by optimization method and deep learning was tested in simulations, and the octorotor successfully followed the given reference angle. © The Author(s), under exclusive licence to The Brazilian Society of Mechanical Sciences and Engineering 2024.
dc.identifier.doi10.1007/s40430-024-04972-1
dc.identifier.eissn1806-3691
dc.identifier.issn1678-5878
dc.identifier.issue6
dc.identifier.scopus2-s2.0-85194184921
dc.identifier.startpage381
dc.identifier.urihttps://rdlopen.rawdatalibrary.net/r/ebyu/11885
dc.identifier.volume46
dc.identifier.wosWOS:001230276200004
dc.language.isoen
dc.publisherSpringer Science and Business Media Deutschland GmbH
dc.relation.ispartofJournal of the Brazilian Society of Mechanical Sciences and Engineering
dc.rightsinfo:eu-repo/semantics/openAccess
dc.subjectDeep neural network
dc.subjectMorphing
dc.subjectOctorotor
dc.subjectPID
dc.subjectSPSA
dc.subjectAircraft control
dc.subjectFlight control systems
dc.subjectOptimization
dc.subjectStochastic control systems
dc.subjectStochastic systems
dc.subjectArm lengths
dc.subjectControl system designs
dc.subjectFlight control
dc.subjectFlight-control systems
dc.subjectOptimal tuning
dc.subjectStochastics
dc.subjectDeep neural networks
dc.titleOctorotor flight control system design with stochastic optimal tuning, deep learning and differential morphing
dc.typeArticle
dspace.entity.typePublication
rdl.citation.scopus6
rdl.citation.wos5
rdl.source.indexSCOPUS
rdl.source.indexWOS
rdl.wos.indexScience Citation Index Expanded (SCI-EXPANDED)