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Design and Flight Tests of a Small Flying Wing UAV

This study presents the design and flight testing of a small unmanned aerial vehicle (UAV) in a flying wing configuration. The flying wing concept provides a low-drag platform suitable for observation, surveillance, and search-and-rescue missions. The UAV is designed to achieve inherent stability wi...

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Principais autores: Witold Zięba, Paweł Rzucidło, Łukasz Wałek
Format: Artigo
Sprog:Inglês
Udgivet: MDPI AG 2026-03-01
Serier:Aerospace
Fag:
flying wing UAV
unmanned aerial vehicle
aerodynamic stability
flight testing
long-endurance flight
low-drag configuration
Online adgang:https://www.mdpi.com/2226-4310/13/3/240
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