CONCEPTUAL DESIGN OF SOLAR UNMANNED AERIAL VEHICLE
Journal Title: Електроніка та системи управління - Year 2018, Vol 2, Issue 56
Abstract
In this paper, emphasis was placed on the fact that a solar unmanned aerial vehicle, should be used in the context of certain missions, taking into account this, the general structure of the aircraft's internal systems was presented. The criterion for continuous flight during the day is analyzed. Based on this, an approach is presented for calculating and modeling the characteristics of a unmanned aerial vehicle, with the possibility of recharging during a daylight solar cycle. The main parameters of the aircraft were the wingspan and aspect ratio of the wing and the capacity of the batteries.
Authors and Affiliations
Denis Karabetsky
Keywords
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- EP ID EP522986
- DOI 10.18372/1990-5548.56.12938
- Views 154
- Downloads 0
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