Page 246 - Neural Network Modeling and Identification of Dynamical Systems

RESULTS OF COMPUTATIONAL EXPERIMENTS WITH ADAPTIVE SYSTEMS 237

FIGURE A.11 The results of a computational experiment for a model reference control system with a compensator for the
stepwise reference signal (hypersonic research vehicle X-43, flight regime M = 6, variant No. 3). 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.