Page 240 - Neural Network Modeling and Identification of Dynamical Systems
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RESULTS OF COMPUTATIONAL EXPERIMENTS WITH ADAPTIVE SYSTEMS      231


















































                          FIGURE A.5 The results of a computational experiment for the MRAC-type control system without the compensator
                          (hypersonic research vehicle X-43, flight mode M = 6). Here α is angle of attack, deg (dotted line for reference model, solid
                          line for plant); E α is tracking error for the given angle of attack, deg; α ref is specifying signal on the angle of attack, deg;
                          δ e, act is command signal for the elevator actuator, deg; t is time, sec.
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