Page 258 - Neural Network Modeling and Identification of Dynamical Systems
P. 258

RESULTS OF COMPUTATIONAL EXPERIMENTS WITH ADAPTIVE SYSTEMS      249



















































                          FIGURE A.23 The results of a computational experiment for the MRAC-type control system (hypersonic research vehicle
                                                              = 0, the reference angle of attack is random. Compensators in both chan-
                          X-43, flight mode M = 6). Constant load factor n x a
                                                                                                             is the
                          nels. II: The reference signals and tracking errors. Here n x a ,ref is the reference signal on tangential load factor; E n xa
                          tracking error for the specified value of the tangential load factor; E α is the tracking error for the specified angle of attack
                          value, deg; α ref is reference signal on the angle of attack, deg; t is time, sec.
   253   254   255   256   257   258   259   260   261   262   263