Page 260 - Neural Network Modeling and Identification of Dynamical Systems
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RESULTS OF COMPUTATIONAL EXPERIMENTS WITH ADAPTIVE SYSTEMS      251




















































                          FIGURE A.25 The results of a computational experiment for the MRAC-type control system (hypersonic research vehicle
                                                              = 0, the reference angle of attack is random. There is no compensator in
                          X-43, flight mode M = 6). Constant load factor n x a
                          the overload channel. II: The reference signals and tracking errors. Here n x a ,ref is the reference signal on tangential load
                                  is the tracking error for the specified value of the tangential load factor; E α is the tracking error for the specified
                          factor; E n xa
                          angle of attack value, deg; α ref is reference signal on the angle of attack, deg; t is time, sec.
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