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256                 RESULTS OF COMPUTATIONAL EXPERIMENTS WITH ADAPTIVE SYSTEMS




















































                         FIGURE A.30 The results of a computational experiment for the MRAC-type control system (hypersonic research vehicle
                         X-43, flight mode M = 6). Both reference signals are random. Compensators in both channels. I: Behavior of the object and
                                               is the tangential load factor; δ th is engine control command signal; α is angle of attack, deg
                         the reference model. Here n x a
                         (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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