dc.contributor.author | Şal, Fırat | |
dc.date.accessioned | 2020-05-24T14:24:17Z | |
dc.date.available | 2020-05-24T14:24:17Z | |
dc.date.issued | 2019 | |
dc.identifier.citation | Şal, F., (2019).Effect of Morphing on Control Energy of Output Variance Constrained Controller for Load-Carrying
UAVs 3rd International Symposium on Multidisciplinary Studies and Innovative Technologies,ISMSIT 2019 - Proceedings, art. no. 8932926. https://doi.org/10.1109/ISMSIT.2019.8932926 | en_US |
dc.identifier.isbn | 9781728137896 | |
dc.identifier.uri | https://doi.org/10.1109/ISMSIT.2019.8932926 | |
dc.identifier.uri | https://hdl.handle.net/20.500.12508/1058 | |
dc.description | 3rd International Symposium on Multidisciplinary Studies and Innovative Technologies, ISMSIT 2019 -- 11 October 2019 through 13 October 2019 -- -- 156063 | en_US |
dc.description.abstract | This paper presents novel results for load-carrying UAVs having morphing capability and guided by output variance constrained controller. Effects of extension ratios of wing span and horizontal tail span on control energy of variance constrained controller satisfying straight level and constant speed flight of load-carrying UAV are in primary scope for this paper. A specific UAV called as ZANKA-II is benefitted and its data is used for these analyses. First of all, dynamic modeling of fixed-wing UAVs is presented and effect of morphing on these models is also emphasized. Then, effect of morphing on control energy of output variance constrained controller for load-carrying UAVs using 3-D Matlab graph is given. Comparisons between control energy versus extension ratios of wing span and horizontal tail span are made. Finally, closed-loop responses for the best scenario is deeply presented and discussed. © 2019 IEEE. | en_US |
dc.description.sponsorship | 214M282 Türkiye Bilimsel ve Teknolojik Araştirma Kurumu | en_US |
dc.description.sponsorship | ACKNOWLEDGMENT This work was supported by Research Fund of The Scientific and Technological Research Council of Turkey (TUBITAK) under Project Number: 214M282. | en_US |
dc.language.iso | eng | en_US |
dc.publisher | Institute of Electrical and Electronics Engineers Inc. | en_US |
dc.relation.isversionof | 10.1109/ISMSIT.2019.8932926 | en_US |
dc.rights | info:eu-repo/semantics/closedAccess | en_US |
dc.subject | closed-loop responses | en_US |
dc.subject | control energy | en_US |
dc.subject | morphing | en_US |
dc.subject | UAVs | en_US |
dc.subject | variance constrained controllers | en_US |
dc.subject.other | Closed-loop responses | en_US |
dc.subject.other | Control energy | en_US |
dc.subject.other | Morphing | en_US |
dc.subject.other | UAVs | en_US |
dc.subject.other | Variance constrained controllers | en_US |
dc.subject.other | Fixed wings | en_US |
dc.subject.other | Unmanned aerial vehicles (UAV) | en_US |
dc.subject.other | Constant speed | en_US |
dc.subject.other | ITS data | en_US |
dc.subject.other | Load carrying | en_US |
dc.subject.other | Morphing capability | en_US |
dc.subject.other | Wing span | en_US |
dc.subject.other | Controllers | en_US |
dc.title | Effect of Morphing on Control Energy of Output Variance Constrained Controller for Load-Carrying UAVs | en_US |
dc.type | conferenceObject | en_US |
dc.relation.journal | 3rd International Symposium on Multidisciplinary Studies and Innovative Technologies, ISMSIT 2019 - Proceedings | en_US |
dc.contributor.department | İskenderun Teknik Üniversitesi | en_US |
dc.contributor.department | Havacılık ve Uzay Bilimleri Fakültesi -- Uçak Bakım ve Onarım Bölümü | |
dc.relation.publicationcategory | Konferans Öğesi - Uluslararası - Kurum Öğretim Elemanı | en_US |
dc.contributor.isteauthor | Şal, Fırat | |