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246                 RESULTS OF COMPUTATIONAL EXPERIMENTS WITH ADAPTIVE SYSTEMS




















































                         FIGURE A.20 The results of a computational experiment for the MRAC-type control system without the compensator (for
                         the hypersonic research vehicle NASP, flight mode M = 6). Here α is angle of attack, deg (dotted line for reference model,
                         solid line for plant); 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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