UAV - Unmanned Aerial Vehicle
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This document outlines the design of an Unmanned Aerial Vehicle (UAV) created in SolidWorks, emphasizing its primary structural components and materials. The UAV features wings made from high-density foam, providing lightweight and aerodynamically efficient support for stable flight. The fuselage is constructed from flexible filament, offering flexibility and resilience to enhance crash resistance and simplify maintenance. The main structure, which supports all components, is made from carbon fiber, ensuring a high strength-to-weight ratio for a robust and durable framework. This combination of materials ensures optimal performance, lightweight, and durability for the UAV.
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