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Critical design parameters for a low altitude long endurance solar powered UAV

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

11 Citations (Scopus)

Abstract

The paper presented provides theoretical findings of the critical solar UAV parameters required for prolonged flight. The parameters being, battery energy density, wing surface area, total UAV weight and solar surface area. The findings are based on two individual models, a solar and an aerodynamic model, which are combined to form a solar powered UAV model.

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

UN SDGs

This output contributes to the following UN Sustainable Development Goals (SDGs)

  1. SDG 7 - Affordable and Clean Energy
    SDG 7 Affordable and Clean Energy

ASJC Scopus subject areas

  • Computer Science Applications
  • Electrical and Electronic Engineering

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