Page 239 - Neural Network Modeling and Identification of Dynamical Systems

230 RESULTS OF COMPUTATIONAL EXPERIMENTS WITH ADAPTIVE SYSTEMS

FIGURE A.4 The results of a computational experiment for the MRAC-type control system with the compensator (hyper-
sonic 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 reference signal on the angle of attack, deg; δ e, act is
command signal for the elevator actuator, deg; t is time, sec.