Remote Control Flying Robo Brid (a.k.a Ornithopter)

Electrical Engineering

This project aims to design, build, and test a prototype ornithopter capable of sustained to flight using flapping wing . The ornithopter was designed based on avian biomechanics principles, with a focus on achieving efficient lift and thrust generation. The prototype was constructed using light weight materials such as carbon fiber and plastic materials , and those connected to the miniature electric motor. Flight tests were conducted to assess the aerodynamic performance of the ornithopter, including measurements of lift, thrust, and power consumption. Results indicate that the ornithopter achieved stable flight and demonstrated promising aerodynamic efficiency. Challenges encountered during the project, such as control system optimization and structural stability, are discussed along with potential avenues for future research. Keywords: Ornithopter, Flapping Wing , Aerodynamics, Prototype Design, Flight Testing.

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