Mathematical modeling and simulation of an unmanned aerial vehicle, specifically, quadrotor modeling is not an easy task because of its complex structure, non linear dynamics and under-actuated nature. In this paper a dynamic model of a quadrotor has been developed using MATLAB/SIMULINK software platform. The aim is to model a quadrotor vehicle as realistic as possible. The model is then used to design a PID controller structure to stabilize the roll, pitch and yaw angles of the quad rotor system. The developed systems id tested successfully for number of numerical simulation runs.
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