I. Introduction
The dynamics of unmanned aircraft systems (UASs) are generally represented using a nonlinear mathematical model described by a set of first order differential equations. For UAS control design purposes, feedback linearization is a well known technique which, under the implementation of an appropriate feedback controller, renders the input-output dynamics of a nonlinear plant linear. Once a linearizing controller has been constructed, desired output trajectories for the nonlinear plant can be tracked using a variety of linear control techniques. However, the calculation of a linearizing controller requires a precise knowledge of the nonlinear dynamic model of the system, which are usually not available or disclosed by the manufacturers of this kind of system.