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234 RESULTS OF COMPUTATIONAL EXPERIMENTS WITH ADAPTIVE SYSTEMS
FIGURE A.8 The results of a computational experiment for a model reference control system with a compensator for an
insufficiently accurate ANN model of the controlled object (hypersonic research vehicle X-43, flight regime M = 6). Here α is
angle of attack, deg (dotted line for reference model, solid line for plant); E α is the angle of attack tracking error, deg; α ref is
the angle of attack reference signal, deg; δ e, act is command signal for the elevator actuator, deg; t is time, sec.
