Page 268 - Neural Network Modeling and Identification of Dynamical Systems
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RESULTS OF COMPUTATIONAL EXPERIMENTS WITH ADAPTIVE SYSTEMS      259


















































                          FIGURE A.33 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 the overload channel. II:
                                                             is tangential load factor error; n x a ,ref is the reference signal on tangential
                          Reference signals and tracking errors. Here E n xa
                          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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