Small fuel cell powering an unmanned aerial vehicle

Marco Klaus Fürrutter, Johan Meyer

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

20 Citations (Scopus)

Abstract

This paper presents the design of a power plant in the form of a 100 W hydrogen fuel cell to provide sufficient power to maintain steady, level flight for a small scale fixed wing unmanned aerial vehicle (UAV). The size of the fuel size is smaller than any other fuel cell previously used for this type of application. What makes this aircraft unique is the small fuel cell, which will be integrated into the UAV to achieve the objective of sustaining flight using only 100 W of power. Performances of the fuel cell and aircraft are evaluated using data from laboratory and flight tests.

Original languageEnglish
Title of host publicationIEEE Africon 2009
DOIs
Publication statusPublished - 2009
EventIEEE Africon 2009 - Nairobi, Kenya
Duration: 23 Sept 200925 Sept 2009

Publication series

NameIEEE AFRICON Conference

Conference

ConferenceIEEE Africon 2009
Country/TerritoryKenya
CityNairobi
Period23/09/0925/09/09

ASJC Scopus subject areas

  • Computer Science Applications
  • Electrical and Electronic Engineering

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