Simulation and control design of a midrange WPT charging system for in-flight drones

Drones, or unmanned aerial vehicles (UAVs), have emerged as an indispensable tool across numerous industries due to their remarkable versatility, efficiency, and capabilities. Not with standing all these traits, drones are still limited by battery life. In this paper, we propose a genuine in-flight...

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Main Authors: Allama, Oussama, Habaebi, Mohamed Hadi, Khan, Sheroz, Islam, Md. Rafiqul, Alghaihab, Abdullah
Format: Article
Language:English
English
Published: Multidisciplinary Digital Publishing Institute (MDPI) 2023
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Online Access:http://irep.iium.edu.my/105908/1/105908_Simulation%20and%20control%20design.pdf
http://irep.iium.edu.my/105908/7/105908_Simulation%20and%20control%20design_Scopus.pdf
http://irep.iium.edu.my/105908/
https://www.mdpi.com/1996-1073/16/15/5746
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spelling my.iium.irep.1059082023-11-02T03:00:36Z http://irep.iium.edu.my/105908/ Simulation and control design of a midrange WPT charging system for in-flight drones Allama, Oussama Habaebi, Mohamed Hadi Khan, Sheroz Islam, Md. Rafiqul Alghaihab, Abdullah TK7800 Electronics. Computer engineering. Computer hardware. Photoelectronic devices Drones, or unmanned aerial vehicles (UAVs), have emerged as an indispensable tool across numerous industries due to their remarkable versatility, efficiency, and capabilities. Not with standing all these traits, drones are still limited by battery life. In this paper, we propose a genuine in-flight charging method without landing. The charging system consists of three orthogonal coils, among which the receiving coil is connected to the drone. The development of the model for wireless dynamic charging systems is achieved by integrating the receiver trajectory and velocity in the model. Furthermore, the model is significantly enhanced by introducing the concept of the positioning mutual coupling function for the receiver trajectory; thus, it is possible to simulate a genuine continuous trajectory for UAVs and link it to the systems’ total input power consumption. The developed control algorithm can direct the magnetic field resultant to track the exact trajectory of the drone. The real-time simulation of the multiparameter discrete extremum-seeking control (ESC) algorithm on the (DSP) F28379D hardware shows that the input power is maximized up to 12Win a response time of 2 ms for a drone-hovering velocity of 8 m/s without any feedback. Multidisciplinary Digital Publishing Institute (MDPI) 2023-08-01 Article PeerReviewed application/pdf en http://irep.iium.edu.my/105908/1/105908_Simulation%20and%20control%20design.pdf application/pdf en http://irep.iium.edu.my/105908/7/105908_Simulation%20and%20control%20design_Scopus.pdf Allama, Oussama and Habaebi, Mohamed Hadi and Khan, Sheroz and Islam, Md. Rafiqul and Alghaihab, Abdullah (2023) Simulation and control design of a midrange WPT charging system for in-flight drones. Energies, 16 (15). pp. 1-19. ISSN 1996-1073 https://www.mdpi.com/1996-1073/16/15/5746 10.3390/en16155746
institution Universiti Islam Antarabangsa Malaysia
building IIUM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider International Islamic University Malaysia
content_source IIUM Repository (IREP)
url_provider http://irep.iium.edu.my/
language English
English
topic TK7800 Electronics. Computer engineering. Computer hardware. Photoelectronic devices
spellingShingle TK7800 Electronics. Computer engineering. Computer hardware. Photoelectronic devices
Allama, Oussama
Habaebi, Mohamed Hadi
Khan, Sheroz
Islam, Md. Rafiqul
Alghaihab, Abdullah
Simulation and control design of a midrange WPT charging system for in-flight drones
description Drones, or unmanned aerial vehicles (UAVs), have emerged as an indispensable tool across numerous industries due to their remarkable versatility, efficiency, and capabilities. Not with standing all these traits, drones are still limited by battery life. In this paper, we propose a genuine in-flight charging method without landing. The charging system consists of three orthogonal coils, among which the receiving coil is connected to the drone. The development of the model for wireless dynamic charging systems is achieved by integrating the receiver trajectory and velocity in the model. Furthermore, the model is significantly enhanced by introducing the concept of the positioning mutual coupling function for the receiver trajectory; thus, it is possible to simulate a genuine continuous trajectory for UAVs and link it to the systems’ total input power consumption. The developed control algorithm can direct the magnetic field resultant to track the exact trajectory of the drone. The real-time simulation of the multiparameter discrete extremum-seeking control (ESC) algorithm on the (DSP) F28379D hardware shows that the input power is maximized up to 12Win a response time of 2 ms for a drone-hovering velocity of 8 m/s without any feedback.
format Article
author Allama, Oussama
Habaebi, Mohamed Hadi
Khan, Sheroz
Islam, Md. Rafiqul
Alghaihab, Abdullah
author_facet Allama, Oussama
Habaebi, Mohamed Hadi
Khan, Sheroz
Islam, Md. Rafiqul
Alghaihab, Abdullah
author_sort Allama, Oussama
title Simulation and control design of a midrange WPT charging system for in-flight drones
title_short Simulation and control design of a midrange WPT charging system for in-flight drones
title_full Simulation and control design of a midrange WPT charging system for in-flight drones
title_fullStr Simulation and control design of a midrange WPT charging system for in-flight drones
title_full_unstemmed Simulation and control design of a midrange WPT charging system for in-flight drones
title_sort simulation and control design of a midrange wpt charging system for in-flight drones
publisher Multidisciplinary Digital Publishing Institute (MDPI)
publishDate 2023
url http://irep.iium.edu.my/105908/1/105908_Simulation%20and%20control%20design.pdf
http://irep.iium.edu.my/105908/7/105908_Simulation%20and%20control%20design_Scopus.pdf
http://irep.iium.edu.my/105908/
https://www.mdpi.com/1996-1073/16/15/5746
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score 13.187197