Abstract
The main purpose of this work was to spear head research and development in Micro Aerial Vehicles (MAVs) especially in the development small flapping wing systems which can greatly be used for defense as well as surveillance purposes. This project focused on the development of a flapping wing mechanism with a wing span of just 3 cm using a piezoelectric bimorph actuator. Keywords: Micro Aerial Vehicles, MAV, Piezoelectric, Bimorph, Actuator, Flapping wing system Cite this Article Nandujith P.J., Vasantha Kumari K.G., Sushanth S., Blesson K., M.S. Prasad N. Raghu.Design and Fabrication of a Piezo Actuated Flapping Mechanism for a Micro Aerial Vehicle. Journal of Aerospace Engineering and Technology. 2017; 7(1): 28–33p.
Sign-in/Register to access full text options 
Free) 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a call
