Dynamic Analysis of Coaxial Rotor Systems

Unmanned aerial vehicles (UAV's), also known as drones, are becoming more popular from being used for military purposes to space exploration. While the current airframes face difficulty in speed, agility, and conformance to purpose, this paper explores the dynamics & forces experienced by the rotor system of a coaxial drone which is still under limited research exposure. The prototype designed here can be used to carry generic payloads that can be adapted for a wide range of applications such as Remote Sens and even for agricultural purposes. This system has better dynamic stability, compact in design, and reduces energy swirl losses.