Flapping Wing Aerial Vehicle

Abstract

This report describes the design, implementation, and testing of a Flapping Wing Aerial Vehicle (FWAV) prototype, which was inspired by the flight mechanism of birds and insects. The FWAV's design offers improved maneuverability and agility compared to traditional aircraft, making it a potential alternative for specific applications. The design process involved aerodynamic analysis, material selection, and component integration. The FWAV prototype was equipped with a microcontroller-based control system that allowed for stable and precise flight control. The prototype underwent extensive testing, demonstrating its capability for stable hovering, forward flight, and turning maneuvers. This project's outcomes offer valuable insights into the design and implementation of a flapping wing aerial vehicle, which has potential applications in various fields such as surveillance, environmental monitoring, and search and rescue operations. The FWAV design provides improved maneuverability and agility, making it particularly useful in applications where traditional aircraft may not be effective. In conclusion, this report demonstrates the feasibility of a flapping wing aerial vehicle as a potential alternative to traditional aircraft for specific applications. The FWAV prototype's stable flight performance validated the design's effectiveness, offering valuable insights into the design and implementation of a flapping wing aerial vehicle.