Paper Title
Design And Control Implementation Of Quadcopter

Quadcopter has extremely developed in the area of research due to its flexibility of takeoff and range of uses. Being simple, small, and cost effective quadcopter is gaining advantage in various applications. The need for Un-manned Aerial Vehicles (UAV) in various fields such as industries, military, nuclear power plant, space exploration, disaster rescue etc. has improved its usage. In this paper quadcopter was modelled and the frame was analyzed for an optimum load. Mathematical modelling & simulation of the system using matlab for stability analysis was conducted. In order to obtain desired response and stability, a tuned PID controller parameters were utilized. Keywords— Quadcopter, Modelling, Simulation, Stability Analysis.