I. Introduction
Milligram-scale flapping wing micro-aerial vehicles (MAVs)have a myriad of applications including, but not limited to, sensor networks, first responders for disasters, reconnaissance, and exploration of new planets. This range of applications is due to their expected insect-like maneuverability, navigation over tough terrains, and potential for swarm behavior, all of it owing to their small size and the promise for mass production. But this size scale also poses a significant challenge in the design of MAVs weighing below 100mg. Only a few designs are known to be capable of lifting their own weight [1]–[4] and except one [4] all do so via tethered operation providing external electric power. High energy density battery, high power actuator, and a mechanism producing large wing stroke angles are some of the major design problems.