“…A secondorder low-pass digital filter should be employed to reduce noise and compute both first and second derivatives of η d [17], so as to getη d andη d , and hence compute in turn the attitude tracking errors e η andė η . The control input vector τ b b is computed as in (15), in which τ u is given by (12). Having both the thrust u and the actuation torques τ b b , the squared propellers speeds w 2 i of the VToL UAV, with i = 1, .…”