Designing hybrid energy source system for long endurance electric UAV

Wojciech Skarka; Magdalena Peciak

doi:10.3233/ATDE190101

Designing hybrid energy source system for long endurance electric UAV

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Abstrakt

The article presents the conceptual design of Hybrid Energy Source System (HESS) for Long Endurance Electric UAV. During the design, the MBD method was used to analyze energy consumption during various UAV operational states as well as the entire mission for different HESS concepts. Such analysis at an early stage of the concept allows you to choose the optimal HESS set for a given UAV and expected mission parameters. The design method is based on a simulation computer model of subsystems and flight phenomena affecting the energy consumption during the flight. The modular construction of the simulation model allows the use of various details of simulation models for different stages of project development. The use of the HESS solution as well as the method of its design makes it possible to overcome the basic inconvenience of using electric drives in all types of vehicles, ie reconciling sufficient temporary operational parameters of the drive and long-term operation. In addition to the description of the method itself and the details of the simulation model, the article also presents a case study for the popular UAV class.

Język oryginału	angielski
Tytuł publikacji goszczącej	Transdisciplinary Engineering for Complex Socio-technical Systems - Proceedings of the 26th ISTE International Conference on Transdisciplinary Engineering
Redaktorzy	Kazuo Hiekata, `Brian Moser, Brian Moser, Masato Inoue, Josip Stjepandic, Nel Wognum
Wydawca	IOS Press BV
Strony	3-11
Liczba stron	9
ISBN (elektroniczny)	9781643680200
Identyfikatory DOI	https://doi.org/10.3233/ATDE190101
Status publikacji	Opublikowano - 7 paź 2019
Wydarzenie	26th ISTE International Conference on Transdisciplinary Engineering, TE 2019 - Tokyo, Japonia Czas trwania: 30 lip 2019 → 1 sie 2019

Seria publikacji

Nazwa	Advances in Transdisciplinary Engineering
Tom	10
ISSN (drukowany)	2352-751X
ISSN (elektroniczny)	2352-7528

Konferencja

Konferencja	26th ISTE International Conference on Transdisciplinary Engineering, TE 2019
Kraj/Terytorium	Japonia
Miejscowość	Tokyo
Okres	30/07/19 → 1/08/19

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/ATDE190101

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Skarka, W., & Peciak, M. (2019). Designing hybrid energy source system for long endurance electric UAV. W K. Hiekata, B. Moser, B. Moser, M. Inoue, J. Stjepandic, & N. Wognum (Red.), Transdisciplinary Engineering for Complex Socio-technical Systems - Proceedings of the 26th ISTE International Conference on Transdisciplinary Engineering (str. 3-11). (Advances in Transdisciplinary Engineering; Tom 10). IOS Press BV. https://doi.org/10.3233/ATDE190101

Skarka, Wojciech ; Peciak, Magdalena. / Designing hybrid energy source system for long endurance electric UAV. Transdisciplinary Engineering for Complex Socio-technical Systems - Proceedings of the 26th ISTE International Conference on Transdisciplinary Engineering. redaktor / Kazuo Hiekata ; `Brian Moser ; Brian Moser ; Masato Inoue ; Josip Stjepandic ; Nel Wognum. IOS Press BV, 2019. str. 3-11 (Advances in Transdisciplinary Engineering).

@inproceedings{4a848c0ea5b349269865ae65963749f4,

title = "Designing hybrid energy source system for long endurance electric UAV",

abstract = "The article presents the conceptual design of Hybrid Energy Source System (HESS) for Long Endurance Electric UAV. During the design, the MBD method was used to analyze energy consumption during various UAV operational states as well as the entire mission for different HESS concepts. Such analysis at an early stage of the concept allows you to choose the optimal HESS set for a given UAV and expected mission parameters. The design method is based on a simulation computer model of subsystems and flight phenomena affecting the energy consumption during the flight. The modular construction of the simulation model allows the use of various details of simulation models for different stages of project development. The use of the HESS solution as well as the method of its design makes it possible to overcome the basic inconvenience of using electric drives in all types of vehicles, ie reconciling sufficient temporary operational parameters of the drive and long-term operation. In addition to the description of the method itself and the details of the simulation model, the article also presents a case study for the popular UAV class.",

keywords = "Hybrid energy source system, Model-based design, Unmanned aerial vehicle",

author = "Wojciech Skarka and Magdalena Peciak",

note = "Publisher Copyright: {\textcopyright} 2019 The authors and IOS Press.; 26th ISTE International Conference on Transdisciplinary Engineering, TE 2019 ; Conference date: 30-07-2019 Through 01-08-2019",

year = "2019",

month = oct,

day = "7",

doi = "10.3233/ATDE190101",

language = "English",

series = "Advances in Transdisciplinary Engineering",

publisher = "IOS Press BV",

pages = "3--11",

editor = "Kazuo Hiekata and `Brian Moser and Brian Moser and Masato Inoue and Josip Stjepandic and Nel Wognum",

booktitle = "Transdisciplinary Engineering for Complex Socio-technical Systems - Proceedings of the 26th ISTE International Conference on Transdisciplinary Engineering",

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Skarka, W & Peciak, M 2019, Designing hybrid energy source system for long endurance electric UAV. w K Hiekata, B Moser, B Moser, M Inoue, J Stjepandic & N Wognum (red), Transdisciplinary Engineering for Complex Socio-technical Systems - Proceedings of the 26th ISTE International Conference on Transdisciplinary Engineering. Advances in Transdisciplinary Engineering, tom 10, IOS Press BV, str. 3-11, 26th ISTE International Conference on Transdisciplinary Engineering, TE 2019, Tokyo, Japonia, 30/07/19. https://doi.org/10.3233/ATDE190101

Designing hybrid energy source system for long endurance electric UAV. / Skarka, Wojciech ; Peciak, Magdalena.
Transdisciplinary Engineering for Complex Socio-technical Systems - Proceedings of the 26th ISTE International Conference on Transdisciplinary Engineering. red. / Kazuo Hiekata; `Brian Moser; Brian Moser; Masato Inoue; Josip Stjepandic; Nel Wognum. IOS Press BV, 2019. str. 3-11 (Advances in Transdisciplinary Engineering; Tom 10).

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

TY - GEN

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AU - Peciak, Magdalena

PY - 2019/10/7

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N2 - The article presents the conceptual design of Hybrid Energy Source System (HESS) for Long Endurance Electric UAV. During the design, the MBD method was used to analyze energy consumption during various UAV operational states as well as the entire mission for different HESS concepts. Such analysis at an early stage of the concept allows you to choose the optimal HESS set for a given UAV and expected mission parameters. The design method is based on a simulation computer model of subsystems and flight phenomena affecting the energy consumption during the flight. The modular construction of the simulation model allows the use of various details of simulation models for different stages of project development. The use of the HESS solution as well as the method of its design makes it possible to overcome the basic inconvenience of using electric drives in all types of vehicles, ie reconciling sufficient temporary operational parameters of the drive and long-term operation. In addition to the description of the method itself and the details of the simulation model, the article also presents a case study for the popular UAV class.

AB - The article presents the conceptual design of Hybrid Energy Source System (HESS) for Long Endurance Electric UAV. During the design, the MBD method was used to analyze energy consumption during various UAV operational states as well as the entire mission for different HESS concepts. Such analysis at an early stage of the concept allows you to choose the optimal HESS set for a given UAV and expected mission parameters. The design method is based on a simulation computer model of subsystems and flight phenomena affecting the energy consumption during the flight. The modular construction of the simulation model allows the use of various details of simulation models for different stages of project development. The use of the HESS solution as well as the method of its design makes it possible to overcome the basic inconvenience of using electric drives in all types of vehicles, ie reconciling sufficient temporary operational parameters of the drive and long-term operation. In addition to the description of the method itself and the details of the simulation model, the article also presents a case study for the popular UAV class.

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Skarka W , Peciak M. Designing hybrid energy source system for long endurance electric UAV. W Hiekata K, Moser B, Moser B, Inoue M, Stjepandic J, Wognum N, redaktorzy, Transdisciplinary Engineering for Complex Socio-technical Systems - Proceedings of the 26th ISTE International Conference on Transdisciplinary Engineering. IOS Press BV. 2019. str. 3-11. (Advances in Transdisciplinary Engineering). doi: 10.3233/ATDE190101

Designing hybrid energy source system for long endurance electric UAV

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Konferencja

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