Zobrazeno 1 - 10 of 29 pro vyhledávání: '"Aziz Kaba"'
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Akademický článek
Unscented Kalman Filter Based Attitude Estimation of a Quadrotor
Autor: Aziz Kaba
Publikováno v: Havacılık ve Uzay Teknolojileri Dergisi, Vol 14, Iss 1, Pp 79-88 (2021)
Quadrotors are well - known unmanned aerial vehicle structures that have some advantages such as hovering, vertical take – off and landing, and low – speed flight. On the other hand, quadrotors are subjected to modeling and sensor uncertainties t
Externí odkaz: https://doaj.org/article/66ad06100dfa420fbba0cf993712946f
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2
Thrust modelling of a target drone engine with nonlinear least – squares estimation based on series expansions
Autor: Aziz Kaba, Ece Yurdusevimli Metin, Onder Turan
Publikováno v: Aircraft Engineering and Aerospace Technology. 95:38-52
Purpose The purpose of this study is to build a high accuracy thrust model under various small turbojet engine shaft speeds by using robust, ordinary, linear and nonlinear least squares estimation methods for target drone applications. Design/methodo
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::46d93891ea5ca5624427c7b870519cbd
https://doi.org/10.1108/aeat-08-2021-0236
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3
Improved particle filter-based estimation of a quadrotor subjected to uncertainties
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
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4
Improved PID rate control of a quadrotor with a convexity-based surrogated model
Autor: Aziz Kaba
Publikováno v: Aircraft Engineering and Aerospace Technology. 93:1287-1301
Purpose The purpose of this paper is to develop, extend and propose an improved proportional integral derivative (PID) rate control of a quadrotor unmanned aerial vehicle based on a convexity-based surrogated firefly algorithm. Design/methodology/app
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::1460def6d667335bbc1b3f319079ddeb
https://doi.org/10.1108/aeat-03-2021-0093
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5
Multi-dimensional energetic performance modeling of an aircraft engine with the aid of enhanced least–squares estimation based genetic algorithm method
Autor: Aziz Kaba, Onder Turan, Hakan Aygun
Publikováno v: Journal of Thermal Analysis and Calorimetry. 147:5913-5935
Aircraft must have reliable and sustainable sources of power systems and must use energy efficiently. Aircraft engine advances have dramatically improved aircraft fuel efficiency. Variable cycle engine (VCE) has been promising in both civil and milit
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::f7985f72d8fefd5cfed8ca4b2a81068b
https://doi.org/10.1007/s10973-021-10922-z
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6
A probabilistic-based analysis for wind distribution determination of a runway
Autor: Ahmet Esat Suzer, Aziz Kaba
Publikováno v: Aircraft Engineering and Aerospace Technology. 93:284-297
Purpose The purpose of this study is to describe precisely the wind speed regime and characteristics of a runway of an International Airport, the north-western part of Turkey. Design methodology approach Three different probability distributions, nam
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::25bba58a597616cddc65527b3c8785f2
https://doi.org/10.1108/aeat-09-2020-0207
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7
A Comparative Study on The Tuning of The PID Flight Controllers Using Swarm Intelligence
Autor: Aziz Kaba
Publikováno v: Volume: 01, Issue: 02 80-91
International Journal of Aviation Science and Technology
QUAVs have some shortcomings in terms of nonlinearities, coupled dynamics, unstable open–loop characteristics, and they are prone to internal and external disturbances. Therefore, control problem of the QUAVs is still an open issue. Designed contro
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::314d05bc4f828013dca54362b88c249f
https://doi.org/10.23890/ijast.vm01is02.0205
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8
Artificial bee colony–based Kalman filter hybridization for three–dimensional position estimation of a quadrotor
Autor: Aziz Kaba, Emre Kiyak
Publikováno v: Aircraft Engineering and Aerospace Technology. 92:1523-1532
Purpose The purpose of this paper is to introduce an artificial bee colony-based Kalman filter algorithm along with an extended objective function to ensure the optimality of the estimator of the quadrotor in the presence of unknown measurement noise
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::1e844ed8f49d22078d4e686b83299712
https://doi.org/10.1108/aeat-01-2020-0015
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10
Feedback linearization control of a quadrotor
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
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