Page 242 - Neural Network Modeling and Identification of Dynamical Systems

RESULTS OF COMPUTATIONAL EXPERIMENTS WITH ADAPTIVE SYSTEMS 233

FIGURE A.7 The results of a computational experiment for the MRAC-type control system without the compensator (top
pair of graphs) and with the compensator (bottom pair of graphs) for the hypersonic research vehicle X-43, flight mode M = 6,
in the event of a failure situation at time t = 20 sec (aircraft center of gravity shift by 5% back). Here α ref is specifying signal
on the angle of attack, deg,; δ e, act is command signal for the elevator actuator, deg; t is time, sec.