Flapping-Wing Micro Air Vehicle (FWMAV)
Our project aims to develop a Micro Air Vehicle (MAV) that derives its thrust and stability from flapping wing mechanisms, as we explore the unconventional lift generation that makes such flight possible. The research-focused side of our project is the Systems Identification Team, which is responsible for investigating the flow field generated by flapping wing mechanisms as well as the thrust they generate. Meanwhile, the Quadflapper Team works to apply this knowledge to perform experiments on, develop, and optimize air vehicles that utilize flapping wings as their sole form of propulsion.


















