dc.contributor.author | Hovenburg, Anthony Reinier | |
dc.contributor.author | Johansen, Tor Arne | |
dc.contributor.author | Storvold, Rune | |
dc.date.accessioned | 2017-12-12T13:56:23Z | |
dc.date.available | 2017-12-12T13:56:23Z | |
dc.date.created | 2017-12-10T14:27:14Z | |
dc.date.issued | 2017 | |
dc.identifier.isbn | 978-1-5090-4495-5 | |
dc.identifier.uri | http://hdl.handle.net/11250/2470852 | |
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. | nb_NO |
dc.language.iso | eng | nb_NO |
dc.publisher | Institute of Electrical and Electronics Engineers (IEEE) | nb_NO |
dc.relation.ispartof | 2017 International Conference on Unmanned Aircraft Systems | |
dc.title | Mission Performance Trade-offs of Battery-powered sUAS | nb_NO |
dc.type | Chapter | nb_NO |
dc.type | Peer reviewed | nb_NO |
dc.description.version | acceptedVersion | nb_NO |
dc.identifier.doi | 10.1109/ICUAS.2017.7991389 | |
dc.identifier.cristin | 1525318 | |
dc.description.localcode | © 2017 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other uses, in any current or future media, including reprinting/republishing this material for advertising or promotional purposes, creating new collective works, for resale or redistribution to servers or lists, or reuse of any copyrighted component of this work in other works. | nb_NO |
cristin.unitcode | 194,63,25,0 | |
cristin.unitname | Institutt for teknisk kybernetikk | |
cristin.ispublished | true | |
cristin.fulltext | postprint | |
cristin.qualitycode | 1 | |