Page 284 - Neural Network Modeling and Identification of Dynamical Systems

RESULTS OF COMPUTATIONAL EXPERIMENTS WITH ADAPTIVE SYSTEMS 275

FIGURE A.49 The results of a computational experiment for the MPC-type control system with 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 reference signal on the angle of attack, deg; δ e, act is command
signal for the elevator actuator, deg; t is time, sec.