Analysis of a hydrogen fuel cell-PV power system for small UAV
This paper investigates the integration of a hybrid power system for a small unmanned aerial vehicle (UAV). The proposed hybrid power system consists of hydrogen fuel cell, photovoltaic panels and battery. The UAV is modeled to have photovoltaic panels covering the wing area, proton exchange membran...
محفوظ في:
| المؤلف الرئيسي: | |
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| مؤلفون آخرون: | |
| التنسيق: | article |
| منشور في: |
2016
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| الموضوعات: | |
| الوصول للمادة أونلاين: | http://hdl.handle.net/11073/16319 |
| الوسوم: |
إضافة وسم
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| _version_ | 1864513435856797696 |
|---|---|
| author | Gadalla, Mohamed |
| author2 | Zafar, Sayem |
| author2_role | author |
| author_facet | Gadalla, Mohamed Zafar, Sayem |
| author_role | author |
| dc.creator.none.fl_str_mv | Gadalla, Mohamed Zafar, Sayem |
| dc.date.none.fl_str_mv | 2016-04-27 2018-11-05T09:11:51Z 2018-11-05T09:11:51Z |
| dc.format.none.fl_str_mv | application/pdf |
| dc.identifier.none.fl_str_mv | Gadalla, Mohamed, and Sayem Zafar. "Analysis of a hydrogen fuel cell-PV power system for small UAV." International Journal of Hydrogen Energy 41, no. 15 (2016): 6422-6432. 0360-3199 http://hdl.handle.net/11073/16319 10.1016/j.ijhydene.2016.02.129 |
| dc.language.none.fl_str_mv | en_US |
| dc.publisher.none.fl_str_mv | Elsevier |
| dc.relation.none.fl_str_mv | International Journal of Hydrogen Energy https://doi.org/10.1016/j.ijhydene.2016.02.129 |
| dc.subject.none.fl_str_mv | Hydrogen fuel cell Unmanned aerial vehicle PV panels Hybrid power system Enhanced endurance UAV |
| dc.title.none.fl_str_mv | Analysis of a hydrogen fuel cell-PV power system for small UAV |
| dc.type.none.fl_str_mv | info:eu-repo/semantics/publishedVersion info:eu-repo/semantics/article |
| description | This paper investigates the integration of a hybrid power system for a small unmanned aerial vehicle (UAV). The proposed hybrid power system consists of hydrogen fuel cell, photovoltaic panels and battery. The UAV is modeled to have photovoltaic panels covering the wing area, proton exchange membrane fuel cell and a lithium-polymer battery. A small UAV is used for the study that has low takeoff weight and small dimensions to make the UAV man-portable. Analyses are conducted using data acquired through bench tests of the power systems and simulations. Using drag, lift and weight values, the power required by the UAV is determined. Best test measurements and simulations are conducted for the maximum required power. The flight performance of the UAV improved with the hybrid power system. The UAV endurance increased from 470 min to 970 min. The research study shows the usefulness of hybrid power system for a small UAV. Finally, the paper also establishes the effectiveness of using renewable energy sources for mobile applications. |
| format | article |
| id | aus_02432b32dcad9cfc7465531aae8da042 |
| identifier_str_mv | Gadalla, Mohamed, and Sayem Zafar. "Analysis of a hydrogen fuel cell-PV power system for small UAV." International Journal of Hydrogen Energy 41, no. 15 (2016): 6422-6432. 0360-3199 10.1016/j.ijhydene.2016.02.129 |
| language_invalid_str_mv | en_US |
| network_acronym_str | aus |
| network_name_str | aus |
| oai_identifier_str | oai:repository.aus.edu:11073/16319 |
| publishDate | 2016 |
| publisher.none.fl_str_mv | Elsevier |
| repository.mail.fl_str_mv | |
| repository.name.fl_str_mv | |
| repository_id_str | |
| spelling | Analysis of a hydrogen fuel cell-PV power system for small UAVGadalla, MohamedZafar, SayemHydrogen fuel cellUnmanned aerial vehiclePV panelsHybrid power systemEnhanced endurance UAVThis paper investigates the integration of a hybrid power system for a small unmanned aerial vehicle (UAV). The proposed hybrid power system consists of hydrogen fuel cell, photovoltaic panels and battery. The UAV is modeled to have photovoltaic panels covering the wing area, proton exchange membrane fuel cell and a lithium-polymer battery. A small UAV is used for the study that has low takeoff weight and small dimensions to make the UAV man-portable. Analyses are conducted using data acquired through bench tests of the power systems and simulations. Using drag, lift and weight values, the power required by the UAV is determined. Best test measurements and simulations are conducted for the maximum required power. The flight performance of the UAV improved with the hybrid power system. The UAV endurance increased from 470 min to 970 min. The research study shows the usefulness of hybrid power system for a small UAV. Finally, the paper also establishes the effectiveness of using renewable energy sources for mobile applications.Elsevier2018-11-05T09:11:51Z2018-11-05T09:11:51Z2016-04-27info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/articleapplication/pdfGadalla, Mohamed, and Sayem Zafar. "Analysis of a hydrogen fuel cell-PV power system for small UAV." International Journal of Hydrogen Energy 41, no. 15 (2016): 6422-6432.0360-3199http://hdl.handle.net/11073/1631910.1016/j.ijhydene.2016.02.129en_USInternational Journal of Hydrogen Energyhttps://doi.org/10.1016/j.ijhydene.2016.02.129oai:repository.aus.edu:11073/163192024-08-22T12:15:41Z |
| spellingShingle | Analysis of a hydrogen fuel cell-PV power system for small UAV Gadalla, Mohamed Hydrogen fuel cell Unmanned aerial vehicle PV panels Hybrid power system Enhanced endurance UAV |
| status_str | publishedVersion |
| title | Analysis of a hydrogen fuel cell-PV power system for small UAV |
| title_full | Analysis of a hydrogen fuel cell-PV power system for small UAV |
| title_fullStr | Analysis of a hydrogen fuel cell-PV power system for small UAV |
| title_full_unstemmed | Analysis of a hydrogen fuel cell-PV power system for small UAV |
| title_short | Analysis of a hydrogen fuel cell-PV power system for small UAV |
| title_sort | Analysis of a hydrogen fuel cell-PV power system for small UAV |
| topic | Hydrogen fuel cell Unmanned aerial vehicle PV panels Hybrid power system Enhanced endurance UAV |
| url | http://hdl.handle.net/11073/16319 |