Page 270 - Neural Network Modeling and Identification of Dynamical Systems
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RESULTS OF COMPUTATIONAL EXPERIMENTS WITH ADAPTIVE SYSTEMS      261



















































                          FIGURE A.35 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. II: Reference
                                                     is tangential load factor error; n x a ,ref is the reference signal on tangential load factor;
                          signals and tracking errors. Here E n xa
                          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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