Abstract
An Unmanned Aerial Vehicles (UAV) quadrotor, which has many applications concerning civilian and military purposes with a high risk mission. This paper deduces the dynamic modeling of UAV and designs a traditional PID controller that controls and stabilizes the quadrotor's attitude around its hover position. The dynamical model and controllers which proposed or compared and verified of a UAV quadrotor were simulated employing MATLAB /Simulink. The quadrotor control was verified by comparing its results with another sliding mode controller results to ensure that the traditional PID controller is efficient.
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