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RESULTS OF COMPUTATIONAL EXPERIMENTS WITH ADAPTIVE SYSTEMS      253


















































                          FIGURE A.27 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 load factor. Compensators
                                                                           is tangential load factor error; n x a ,ref is the reference
                          in both channels. II: Reference signals and tracking errors. Here E n xa
                          signal on tangential load factor; E α is tracking error for the reference angle of attack, deg; α ref is the reference signal on the
                          angle of attack, deg; t is time, sec.
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