Abstract - An Unmanned Aerial Vehicle (UAV), commonly known as a drone, is an aircraft that operates without a human pilot onboard and is controlled either remotely or autonomously. UAVs serve various applications, from defence to civilian purposes, and are categorized into fixed-wing, rotary-wing, hybrid, nano, tactical, target, and commercial drones. For this project, we selected a quadcopter due to its versatility, stability, and efficiency, making it ideal for applications like surveillance, aerial photography, emergency response, and environmental monitoring. The prototype is modeled in Fusion 360 for precise design and analyzed using ANSYS to assess structural integrity and durability under varying load conditions. The UAV frame is fabricated using lightweight materials such as carbon fiber and integrates key components like brushless DC motors, LiPo batteries, GPS modules, and a Pixhawk flight controller. Advanced features such as real-time data acquisition, autonomous flight capabilities, and efficient payload handling enhance its functionality. Additionally, 3D printing is used for custom parts, ensuring an optimized weight-to-strength ratio. To validate performance, the UAV undergoes simulation of flight dynamics and control systems using SolidWorks, followed by extensive ground and flight testing. The results demonstrate reliable performance in real-world scenarios such as medical supply delivery, environmental condition monitoring, and disaster relief efforts. By leveraging artificial intelligence, real-time data processing, and robust communication networks, this project contributes to the advancement of UAV technology, providing a cost-effective, efficient, and sustainable solution for public services and community needs. Key Words: Unmanned Aerial Vehicle (UAV), Quadcopter, Prototype Development, Structural Integrity, Environmental Monitoring.
Vardhan et al. (Thu,) studied this question.