Page 264 - Neural Network Modeling and Identification of Dynamical Systems

RESULTS OF COMPUTATIONAL EXPERIMENTS WITH ADAPTIVE SYSTEMS 255

FIGURE A.29 The results of a computational experiment for the MRAC-type control system (hypersonic research vehicle
X-43, flight mode M = 6). Constant predetermined angle of attack α = 2 deg, random reference overload. There is no com-
pensator in the overload channel. II: Reference signals and tracking errors. Here E n xa is tangential load factor error; n x a ,ref
is the reference signal on tangential load factor; E α is tracking error for the reference angle of attack, deg; α ref is the reference
signal on the angle of attack, deg; t is time, sec.