Page 253 - Neural Network Modeling and Identification of Dynamical Systems
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244                 RESULTS OF COMPUTATIONAL EXPERIMENTS WITH ADAPTIVE SYSTEMS

















































                         FIGURE A.18 Efficiency verification of the neurocontroller on the test set (for the hypersonic research vehicle NASP, 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; t is time, sec.
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