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254                 RESULTS OF COMPUTATIONAL EXPERIMENTS WITH ADAPTIVE SYSTEMS



















































                         FIGURE A.28 The results of a computational experiment for the MRAC-type control system (hypersonic research vehicle
                         X-43, flight mode M = 6). Constant predetermined angle of attack α = 2 deg, random reference overload. There is no com-
                                                                                             is the tangential load factor;
                         pensator in the overload channel. I: Behavior of the object and the reference model. Here n x a
                         δ th is engine control command signal; α is angle of attack, deg (dotted line for reference model, solid line for plant); δ e, act is
                         command signal for the elevator actuator, deg; t is time, sec.
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