Page 292 - Neural Network Modeling and Identification of Dynamical Systems

RESULTS OF COMPUTATIONAL EXPERIMENTS WITH ADAPTIVE SYSTEMS 283

FIGURE A.57 Results of a computational experiment on the evaluation of the nature of the effect on the controlled system
of atmospheric turbulence: the MRAC-type control system with PD compensator. No perturbing effect. Flight mode H =
100 m, V = 600 km/h. Here α is angle of attack, deg (dotted line for reference model, solid line for plant); α rm is the angle of
attack at the output of the reference model, deg; E α is tracking error for the given angle of attack, deg; α rm is reference signal
on angle of attack, deg; n z is the normal G-load; δ e, act is command signal for actuator of the elevator, deg; t is time, sec.