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.