| dc.contributor.author | Hovenburg, Anthony Reinier | |
| dc.contributor.author | Johansen, Tor Arne | |
| dc.contributor.author | Storvold, Rune | |
| dc.date.accessioned | 2022-10-25T07:33:20Z | |
| dc.date.available | 2022-10-25T07:33:20Z | |
| dc.date.issued | 2017-07-27 | |
| dc.description.abstract | A sensitivity analysis is presented on the influence of the weight, altitude and speed of battery-powered sUAS on the resulting stall speed, endurance and range. To aid in the determination of the aircraft performance prior to flight, a method is being brought forth that quantifies the impact of these mission parameters. As a case study the P31015 sUAS is used. The P31015 is a concept model of a battery-powered sUAS with a total battery capacity of 977Wh. Since the aerodynamic model of the aircraft was determined through simulations, and the specific propulsion set-up is yet to be determined, the case study remains to be a theoretical approach. The proposed methods and limitations of this study are applicable to other electric sUAS in similar set-up. | en_US |
| dc.identifier.citation | Hovenburg AR, Johansen TA, Storvold R: Mission Performance Trade-offs of Battery-powered sUAS. In: Valavanis KP. 2017 International Conference on Unmanned Aircraft Systems, 2017. IEEE | en_US |
| dc.identifier.cristinID | FRIDAID 1525318 | |
| dc.identifier.doi | 10.1109/ICUAS.2017.7991389 | |
| dc.identifier.isbn | 978-1-5090-4495-5 | |
| dc.identifier.uri | https://hdl.handle.net/10037/27125 | |
| dc.language.iso | eng | en_US |
| dc.publisher | IEEE | en_US |
| dc.rights.accessRights | openAccess | en_US |
| dc.title | Mission Performance Trade-offs of Battery-powered sUAS | en_US |
| dc.type.version | acceptedVersion | en_US |
| dc.type | Chapter | en_US |
| dc.type | Bokkapittel | en_US |
English
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