This paper presents the design of a robust control applying the Quantitative Feedback Theory (QFT), for an unmanned aerial vehicle, quadrotor type, equipped with inertial sensors that determine the angle of inclination and the angular velocity. It illustrates the methodology that follows this type of control by design the respective robust controller. This is considered has the possibility to manage a plant, regardless of the presence of uncertainties given by the mathematical model and the projected perturbations. The controller was implemented using rapid prototyping techniques, a process that refers to software and hardware techniques required to reduce the development time and the implementation of control systems, using a high level of abstraction in programming. A controlled environment was available to validate the quadrotor controller; it was subjected to rapid settling times in the presence of perturbations.