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260                 RESULTS OF COMPUTATIONAL EXPERIMENTS WITH ADAPTIVE SYSTEMS



















































                         FIGURE A.34 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 stepwise. There is no compensator in both channels. I: Behavior
                                                           is the tangential load factor; δ th is engine control command signal; α is angle
                         of the object and the reference model. Here n x a
                         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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