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RESULTS OF COMPUTATIONAL EXPERIMENTS WITH ADAPTIVE SYSTEMS      245


















































                          FIGURE A.19 The results of a computational experiment for the MRAC-type control system with 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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