Abstract
<p>This paper work focused on the study of the nonlinear computed torque<br />control of a quadrotor helicopter. In order to model the dynamic of the<br />vehicles, kinematics and dynamics modeling of the X4 is presented. Euler<br />angles and parameters are used in the formulation of this model and the<br />technique of Computed Torque control is introduced. In the second part of<br />the paper, we develop a methodology of control that allows the quadrotor to<br />accomplish a prospecting mission of an environment, as the follow-up of a<br />trajectory by the simulation. Results show that Computed Torque control<br />method is suitable for X4.</p>
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