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280                 RESULTS OF COMPUTATIONAL EXPERIMENTS WITH ADAPTIVE SYSTEMS




















































                         FIGURE A.54 The results of a computational experiment for the MPC-type control system with compensator (micro-UAV
                         “003”), a flight with airspeed V ind = 30 km/h in normal operation conditions. Here α is angle of attack, deg (dotted line for
                         reference model, solid line for plant); E α is tracking error for the given angle of attack, deg; α ref is reference signal on the
                         angle of attack, deg; δ e, act is command signal for the elevator actuator, deg; t is time, sec.
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