“…In order to design the control signals u 2 and u 3 , a desired reference signal is first defined for the angles φ and θ, this is φ d and θ d , respectively. For doing this, we adopt the small angle approximation widely used in the literature of unmanned aerial vehicles (see for example [28,30]). Under this assumption, the dynamics (24), (25), (27)-(29) take the form…”