Design of the power supply system for vertical take-off and landing unmanned aerial vehicle

Jakub Czech; Wojciech Skarka

doi:10.3233/ATDE210124

Design of the power supply system for vertical take-off and landing unmanned aerial vehicle

Jakub Czech
, Wojciech Skarka

Katedra Podstaw Konstrukcji Maszyn (RMT/RMT6)

Silesian University of Technology

Wyniki badań: Rozdział w książce/raport/materiał konferencyjny › Wkład w konferencję › recenzja

Abstrakt

The article presents an analysis of the possibilities of supporting the Vertical Take off and Landing Unmanned Aerial Vehicle electric power systems by using photovoltaic cells. A typical commercial VTOL class drone with electric power was selected for analysis. Concepts of power supply supported by photovoltaic cells have been developed. Analysis of the potential change in performance through the use of such support are presented on the basis of the UAV simulation model and the model-based design. The simulation model takes into account not only the flight parameters of the drone, but also the drive system with the power supply system and the assumed variable lighting parameters. Such a multidisciplinary model was used to analyse the functional parameters. The analysis also includes hypothetical changes in the performance parameters of photovoltaic cells and their impact on the change in UAV performance as well as the impact of changes in the airframe geometry on the profitability of using such a solution.

Język oryginału	angielski
Tytuł publikacji goszczącej	Transdisciplinary Engineering for Resilience
Podtytuł publikacji goszczącej	Responding to System Disruptions - Proceedings of the 28th ISTE International Conference on Transdisciplinary Engineering
Redaktorzy	Linda Newnes, Susan Lattanzio, Bryan R. Moser, Bryan R. Moser, Stjepandic Josip, Nel Wognum
Wydawca	IOS Press BV
Strony	445-454
Liczba stron	10
ISBN (elektroniczny)	9781643682082
Identyfikatory DOI	https://doi.org/10.3233/ATDE210124
Status publikacji	Opublikowano - 20 paź 2021
Wydarzenie	28th ISTE International Conference on Transdisciplinary Engineering, TE 2021 - Virtual, Online, Wielka Brytania Czas trwania: 5 lip 2021 → 9 lip 2021

Seria publikacji

Nazwa	Advances in Transdisciplinary Engineering
Tom	16
ISSN (drukowany)	2352-751X
ISSN (elektroniczny)	2352-7528

Konferencja

Konferencja	28th ISTE International Conference on Transdisciplinary Engineering, TE 2021
Kraj/Terytorium	Wielka Brytania
Miejscowość	Virtual, Online
Okres	5/07/21 → 9/07/21

Cele SDG ONZ

Ten wynik przyczynia się do realizacji następujących celów zrównoważonego rozwoju

Cel 7 Przystępna i czysta energia

Obszary tematyczne ASJC Scopus

Zastosowania informatyki
Inżynieria przemysłowa i produkcyjna
Oprogramowanie
Algebra i teoria liczb
Strategia i zarządzanie

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10.3233/ATDE210124

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Link do publikacji w Scopus

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Czech, J., & Skarka, W. (2021). Design of the power supply system for vertical take-off and landing unmanned aerial vehicle. W L. Newnes, S. Lattanzio, B. R. Moser, B. R. Moser, S. Josip, & N. Wognum (Red.), Transdisciplinary Engineering for Resilience: Responding to System Disruptions - Proceedings of the 28th ISTE International Conference on Transdisciplinary Engineering (str. 445-454). (Advances in Transdisciplinary Engineering; Tom 16). IOS Press BV. https://doi.org/10.3233/ATDE210124

Czech, Jakub ; Skarka, Wojciech. / Design of the power supply system for vertical take-off and landing unmanned aerial vehicle. Transdisciplinary Engineering for Resilience: Responding to System Disruptions - Proceedings of the 28th ISTE International Conference on Transdisciplinary Engineering. redaktor / Linda Newnes ; Susan Lattanzio ; Bryan R. Moser ; Bryan R. Moser ; Stjepandic Josip ; Nel Wognum. IOS Press BV, 2021. str. 445-454 (Advances in Transdisciplinary Engineering).

@inproceedings{7def30356b74452b9b23d418046fb3d9,

title = "Design of the power supply system for vertical take-off and landing unmanned aerial vehicle",

abstract = "The article presents an analysis of the possibilities of supporting the Vertical Take off and Landing Unmanned Aerial Vehicle electric power systems by using photovoltaic cells. A typical commercial VTOL class drone with electric power was selected for analysis. Concepts of power supply supported by photovoltaic cells have been developed. Analysis of the potential change in performance through the use of such support are presented on the basis of the UAV simulation model and the model-based design. The simulation model takes into account not only the flight parameters of the drone, but also the drive system with the power supply system and the assumed variable lighting parameters. Such a multidisciplinary model was used to analyse the functional parameters. The analysis also includes hypothetical changes in the performance parameters of photovoltaic cells and their impact on the change in UAV performance as well as the impact of changes in the airframe geometry on the profitability of using such a solution.",

keywords = "Aircraft design, Model-Based Design, Photovoltaic cells, Power supply, Simulation model, VTOL UAV",

author = "Jakub Czech and Wojciech Skarka",

note = "Publisher Copyright: {\textcopyright} 2021 The authors and IOS Press.; 28th ISTE International Conference on Transdisciplinary Engineering, TE 2021 ; Conference date: 05-07-2021 Through 09-07-2021",

year = "2021",

month = oct,

day = "20",

doi = "10.3233/ATDE210124",

language = "English",

series = "Advances in Transdisciplinary Engineering",

publisher = "IOS Press BV",

pages = "445--454",

editor = "Linda Newnes and Susan Lattanzio and Moser, \{Bryan R.\} and Moser, \{Bryan R.\} and Stjepandic Josip and Nel Wognum",

booktitle = "Transdisciplinary Engineering for Resilience",

address = "Netherlands",

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Czech, J & Skarka, W 2021, Design of the power supply system for vertical take-off and landing unmanned aerial vehicle. w L Newnes, S Lattanzio, BR Moser, BR Moser, S Josip & N Wognum (red), Transdisciplinary Engineering for Resilience: Responding to System Disruptions - Proceedings of the 28th ISTE International Conference on Transdisciplinary Engineering. Advances in Transdisciplinary Engineering, tom 16, IOS Press BV, str. 445-454, 28th ISTE International Conference on Transdisciplinary Engineering, TE 2021, Virtual, Online, Wielka Brytania, 5/07/21. https://doi.org/10.3233/ATDE210124

Design of the power supply system for vertical take-off and landing unmanned aerial vehicle. / Czech, Jakub; Skarka, Wojciech.
Transdisciplinary Engineering for Resilience: Responding to System Disruptions - Proceedings of the 28th ISTE International Conference on Transdisciplinary Engineering. red. / Linda Newnes; Susan Lattanzio; Bryan R. Moser; Bryan R. Moser; Stjepandic Josip; Nel Wognum. IOS Press BV, 2021. str. 445-454 (Advances in Transdisciplinary Engineering; Tom 16).

Wyniki badań: Rozdział w książce/raport/materiał konferencyjny › Wkład w konferencję › recenzja

TY - GEN

T1 - Design of the power supply system for vertical take-off and landing unmanned aerial vehicle

AU - Czech, Jakub

AU - Skarka, Wojciech

PY - 2021/10/20

Y1 - 2021/10/20

N2 - The article presents an analysis of the possibilities of supporting the Vertical Take off and Landing Unmanned Aerial Vehicle electric power systems by using photovoltaic cells. A typical commercial VTOL class drone with electric power was selected for analysis. Concepts of power supply supported by photovoltaic cells have been developed. Analysis of the potential change in performance through the use of such support are presented on the basis of the UAV simulation model and the model-based design. The simulation model takes into account not only the flight parameters of the drone, but also the drive system with the power supply system and the assumed variable lighting parameters. Such a multidisciplinary model was used to analyse the functional parameters. The analysis also includes hypothetical changes in the performance parameters of photovoltaic cells and their impact on the change in UAV performance as well as the impact of changes in the airframe geometry on the profitability of using such a solution.

AB - The article presents an analysis of the possibilities of supporting the Vertical Take off and Landing Unmanned Aerial Vehicle electric power systems by using photovoltaic cells. A typical commercial VTOL class drone with electric power was selected for analysis. Concepts of power supply supported by photovoltaic cells have been developed. Analysis of the potential change in performance through the use of such support are presented on the basis of the UAV simulation model and the model-based design. The simulation model takes into account not only the flight parameters of the drone, but also the drive system with the power supply system and the assumed variable lighting parameters. Such a multidisciplinary model was used to analyse the functional parameters. The analysis also includes hypothetical changes in the performance parameters of photovoltaic cells and their impact on the change in UAV performance as well as the impact of changes in the airframe geometry on the profitability of using such a solution.

KW - Aircraft design

KW - Model-Based Design

KW - Photovoltaic cells

KW - Power supply

KW - Simulation model

KW - VTOL UAV

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DO - 10.3233/ATDE210124

M3 - Conference contribution

AN - SCOPUS:85119213819

T3 - Advances in Transdisciplinary Engineering

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EP - 454

BT - Transdisciplinary Engineering for Resilience

A2 - Newnes, Linda

A2 - Lattanzio, Susan

A2 - Moser, Bryan R.

A2 - Josip, Stjepandic

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PB - IOS Press BV

T2 - 28th ISTE International Conference on Transdisciplinary Engineering, TE 2021

Y2 - 5 July 2021 through 9 July 2021

ER -

Czech J, Skarka W. Design of the power supply system for vertical take-off and landing unmanned aerial vehicle. W Newnes L, Lattanzio S, Moser BR, Moser BR, Josip S, Wognum N, redaktorzy, Transdisciplinary Engineering for Resilience: Responding to System Disruptions - Proceedings of the 28th ISTE International Conference on Transdisciplinary Engineering. IOS Press BV. 2021. str. 445-454. (Advances in Transdisciplinary Engineering). doi: 10.3233/ATDE210124

Design of the power supply system for vertical take-off and landing unmanned aerial vehicle

Abstrakt

Seria publikacji

Konferencja

Cele SDG ONZ

Obszary tematyczne ASJC Scopus

Uzyskaj dostęp do dokumentu

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