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RESULTS OF COMPUTATIONAL EXPERIMENTS WITH ADAPTIVE SYSTEMS      239

















































                          FIGURE A.13 The results of a computational experiment for the MRAC-type control system with compensator (F-16
                          aircraft, flight mode with a test speed V ind = 300 km/h). Adaptation to the change in the dynamics of the controlled object:
                          backwards shift of the center by 10% (t = 30 sec); 50% decrease in the effectiveness of the control (t = 50 sec). Here α is angle
                          of attack, deg (dotted line for reference model, solid line for plant); E α is tracking error for the reference angle of attack, deg;
                          δ e is the deflection angle of the stabilizer, deg; t is time, sec.
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