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248                 RESULTS OF COMPUTATIONAL EXPERIMENTS WITH ADAPTIVE SYSTEMS



















































                         FIGURE A.22 The results of a computational experiment for the MRAC-type control system (hypersonic research vehicle
                                                             = 0, the reference angle of attack is random. Compensators in both chan-
                         X-43, flight mode M = 6). Constant load factor n x a
                                                                       is the tangential load factor; δ th is engine control command
                         nels. I: Behavior of the object and the reference model. Here n x a
                         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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