This paper examines the design aspects of small unmanned aerial vehicles (UAVs) in tandem wing configuration. This type of wing configuration is gaining increasing attention due to its enhanced capabilities of stability, maneuverability, and efficiency. Through a detailed analysis of the main design aspects, this paper explores the integration of tandem wing configurations in small UAVs. The results and conclusions presented here aim to provide useful guidance into optimizing performance and improving operational characteristics of these aerial systems.
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BUICAN et al. (2024) studied this question.
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