Simultaneous autonomous system and powerplant design for morphing quadrotors

MakaleYalnız künye
  • SDG 7 · Erişilebilir ve Temiz Enerji
  • SDG 9 · Sanayi, Yenilikçilik ve Altyapı

Özet

Purpose This study aims to optimize autonomous performance (i.e. both longitudinal and lateral) and endurance of the quadrotor type aerial vehicle simultaneously depending on the autopilot gain coefficients and battery weight. Design/methodology/approach Quadrotor design processes are critical to performance. Unmanned aerial vehicle durability is an important performance parameter. One of the factors affecting durability is the battery. Battery weight, energy capacity and discharge rate are important design parameters of the battery. In this study, proper autopilot gain coefficients and battery weight are obtained by using a stochastic optimization method named as simultaneous perturbation stochastic approximation (SPSA). Because there is no direct correlation between battery weight and battery energy density, artificial neural network (ANN) is benefited to obtain battery energy density corresponding to resulted battery weight found from SPSA algorithm. By using the SPSA algorithm optimum performance index is obtained, then obtained data is used for longitudinal and lateral autonomous flight simulations. Findings With SPSA, the best proportional integrator and derivative (PID) coefficients and battery weight, energy efficiency and endurance were obtained in case of morphing. Research limitations/implications It takes a long time to find the most suitable battery values depending on quadrotor endurance. However, this situation can be overcome with the proposed SPSA. Practical implications It is very useful to determine quadrotor endurance, PID coefficients and morphing rate using the optimization method. Social implications Determining quadrotor endurance, PID coefficients and morphing rate using the optimization method provides advantages in terms of time, cost and practicality. Originality/value The proposed method improves quadrotor endurance. In addition, with the SPSA optimization method and ANN, the parameters required for endurance will be obtained faster and more securely. In addition, the energy density according to the battery weight also contributes to the clean environment and energy efficiency.

Anahtar Kelimeler

RDL Kalıcı Bağlantı (PID)
https://rdlopen.rawdatalibrary.net/r/gumushane/16174Resmi atıflarda kullanılan kalıcı adres
DOI
https://doi.org/10.1108/aeat-06-2021-0180Yayıncı resmi DOI adresi
Tam Kayıt
AlanDeğerDil
dc.contributor.authorSahin, Huseyin
dc.contributor.authorKose, Oguz
dc.contributor.authorOktay, Tugrul
dc.date.accessioned2026-10-22T10:29:02.018301171Z
dc.date.available2026-10-22T10:29:02.018301171Z
dc.date.issued2022-08
dc.description.abstractPurpose This study aims to optimize autonomous performance (i.e. both longitudinal and lateral) and endurance of the quadrotor type aerial vehicle simultaneously depending on the autopilot gain coefficients and battery weight. Design/methodology/approach Quadrotor design processes are critical to performance. Unmanned aerial vehicle durability is an important performance parameter. One of the factors affecting durability is the battery. Battery weight, energy capacity and discharge rate are important design parameters of the battery. In this study, proper autopilot gain coefficients and battery weight are obtained by using a stochastic optimization method named as simultaneous perturbation stochastic approximation (SPSA). Because there is no direct correlation between battery weight and battery energy density, artificial neural network (ANN) is benefited to obtain battery energy density corresponding to resulted battery weight found from SPSA algorithm. By using the SPSA algorithm optimum performance index is obtained, then obtained data is used for longitudinal and lateral autonomous flight simulations. Findings With SPSA, the best proportional integrator and derivative (PID) coefficients and battery weight, energy efficiency and endurance were obtained in case of morphing. Research limitations/implications It takes a long time to find the most suitable battery values depending on quadrotor endurance. However, this situation can be overcome with the proposed SPSA. Practical implications It is very useful to determine quadrotor endurance, PID coefficients and morphing rate using the optimization method. Social implications Determining quadrotor endurance, PID coefficients and morphing rate using the optimization method provides advantages in terms of time, cost and practicality. Originality/value The proposed method improves quadrotor endurance. In addition, with the SPSA optimization method and ANN, the parameters required for endurance will be obtained faster and more securely. In addition, the energy density according to the battery weight also contributes to the clean environment and energy efficiency.
dc.description.sponsorshipErciyes University [FDK-2020-10173, FBA-2020-10102]
dc.identifier.doi10.1108/aeat-06-2021-0180
dc.identifier.eissn1758-4213
dc.identifier.endpage1241
dc.identifier.issn1748-8842
dc.identifier.issue8
dc.identifier.startpage1228
dc.identifier.urihttps://rdlopen.rawdatalibrary.net/r/gumushane/16174
dc.identifier.volume94
dc.identifier.wosWOS:000772473100001
dc.language.isoen
dc.publisherEMERALD GROUP PUBLISHING LTD
dc.relation.ispartofAIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.subjectQuadrotor
dc.subjectSPSA
dc.subjectMorphing
dc.subjectEndurance
dc.subjectPID
dc.subjectOptimization
dc.subjectANN
dc.subject.classificationEngineering, Aerospace
dc.subject.classificationEngineering
dc.subject.otherELECTRIC PROPULSION SYSTEM
dc.subject.otherOPTIMIZATION
dc.titleSimultaneous autonomous system and powerplant design for morphing quadrotors
dc.typeArticle
dspace.entity.typePublication
rdl.citation.openalex43
rdl.citation.wos40
rdl.oa.statusclosed
rdl.sdgSDG07
rdl.sdgSDG09
rdl.source.indexWOS
rdl.wos.indexScience Citation Index Expanded (SCI-EXPANDED)