Zobrazeno 1 - 8
of 8
pro vyhledávání: '"Ahmet Ermeydan"'
Autor:
Ahmet Ermeydan
Publikováno v:
Havacılık ve Uzay Teknolojileri Dergisi, Vol 17, Iss 1, Pp 159-175 (2024)
In this study, proportional controller design isperformedfor different scenarios using a nonlinear quadrotormodel. The state-space model of the quadrotor, whose flight principles areexplained,and equations of motionaresummarized, isobtained usinga Ta
Externí odkaz:
https://doaj.org/article/a13f0565feef44b2a665a17049bc9ddb
Autor:
Aziz Kaba, Ahmet Ermeydan
Publikováno v:
Aircraft Engineering and Aerospace Technology. 94:1144-1156
PurposeThe purpose of this paper is to present an improved particle filter-based attitude estimator for a quadrotor unmanned aerial vehicle (UAV) that addresses the degeneracy issues.Design/methodology/approachControl of a quadrotor is not sufficient
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::37c2295ee693c36fbdbde4d4fe6e601c
https://doi.org/10.1108/aeat-08-2021-0234
https://doi.org/10.1108/aeat-08-2021-0234
Autor:
Aziz Kaba, Ahmet Ermeydan
Publikováno v:
2021 5th International Symposium on Multidisciplinary Studies and Innovative Technologies (ISMSIT).
Quadrotors have a wide range of application areas from aerial mapping to climate observation. However they have some disadvantages such as nonlinear model, coupled dynamics and unstable open – loop characteristics. So, control problem for the quadr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2b25a0d241d6cfdfb5593aec7fec5e04
https://doi.org/10.1109/ismsit52890.2021.9604617
https://doi.org/10.1109/ismsit52890.2021.9604617
Autor:
Emre Kiyak, Ahmet Ermeydan
Publikováno v:
SNE Simulation Notes Europe. 28:85-88
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5ba5bdbb574b49748df212737a418566
https://doi.org/10.11128/sne.28.sn.10422
https://doi.org/10.11128/sne.28.sn.10422
Autor:
Emre Kiyak, Ahmet Ermeydan
Publikováno v:
Aircraft Engineering and Aerospace Technology. 89:468-476
WOS: 000404735800011
Purpose - The purpose of this paper is to present fault tolerant control of a quadrotor based on the enhanced proportional integral derivative (PID) structure in the presence of one or more actuator faults. Design/methodolog
Purpose - The purpose of this paper is to present fault tolerant control of a quadrotor based on the enhanced proportional integral derivative (PID) structure in the presence of one or more actuator faults. Design/methodolog
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6acb04470114d26e4f7a932aba4b5a9b
https://doi.org/10.1108/aeat-04-2015-0096
https://doi.org/10.1108/aeat-04-2015-0096
4th International Conference on Electrical and Electronic Engineering (ICEEE) -- APR 08-10, 2017 -- Ankara, TURKEY
WOS: 000403406400040
Recently unmanned aerial vehicles have become one of the most interesting research topics among scientis
WOS: 000403406400040
Recently unmanned aerial vehicles have become one of the most interesting research topics among scientis
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::39abcd4ad36cde0d35ced41b05dc3cc5
https://hdl.handle.net/11421/18637
https://hdl.handle.net/11421/18637
Autor:
Ahmet Ermeydan, Emre Kiyak
Publikováno v:
Volume: 32, Issue: 1
Gazi Üniversitesi Mühendislik Mimarlık Fakültesi Dergisi
Gazi Üniversitesi Mühendislik Mimarlık Fakültesi Dergisi
Bu çalışmada bir döner kanatın farklı motor arıza senaryolarının geliştirilmiş PID denetleyici yaklaşımıyla arıza toleranslı kontrolü yapılmıştır. Denklemleri verilen hava aracının motor dinamikleri de modellenerek gerçekçi b
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6ac0d28b865eb9401cb3d97e6e315e55
https://dergipark.org.tr/tr/pub/gazimmfd/issue/28296/300591
https://dergipark.org.tr/tr/pub/gazimmfd/issue/28296/300591
Autor:
Emre Kiyak, Ahmet Ermeydan
Publikováno v:
International Journal of Sustainable Aviation. 2:309
WOS: 000410650000004
In this paper a fault tolerant control strategy for a quadrotor is proposed in the presence of actuator faults. A linear mathematical model which is derived from nonlinear model by calculating the Jacobian matrix of the syst
In this paper a fault tolerant control strategy for a quadrotor is proposed in the presence of actuator faults. A linear mathematical model which is derived from nonlinear model by calculating the Jacobian matrix of the syst
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1f9581f1069a98c3962219c3a21420ae
https://doi.org/10.1504/ijsa.2016.082198
https://doi.org/10.1504/ijsa.2016.082198