Page 295 - Neural Network Modeling and Identification of Dynamical Systems

286 RESULTS OF COMPUTATIONAL EXPERIMENTS WITH ADAPTIVE SYSTEMS

FIGURE A.60 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. Perturbing effect: V y,turb in the range
±20 m/sec; q turb in the range ±2 deg/sec. 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.