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6                NEURAL NETWORK MODELING AND IDENTIFICATION OF DYNAMICAL SYSTEMS

                         problem is solved, as a result of which we get the  of ensuring their resistance to changes in the
                         ANN representation for the aerodynamic drag  properties of the object due to failures and dam-
                         coefficient of the maneuverable aircraft.     ages; (3) an assessment of the nature of the im-
                            The Appendix presents the results of numer-  pact of atmospheric turbulence on the controlled
                         ous computational experiments with adaptive  system of the class under consideration; (4) an
                         systems of MRAC and MPC types with refer-    assessment of the possibilities of adaptation of
                         ence to aircraft of various classes. These results  the systems under consideration to uncertain-
                         provideanadequaterepresentationoftopics      ties in the source data; and (5) assessment of the
                         such as (1) the effect of individual structural el-  importance of adaptation mechanisms on the ex-
                         ements of these systems and the properties of  ample of the problem of controlling the angular
                         these elements on the characteristics of the syn-  motion of the aircraft.
                         thesized systems; (2) the capabilities of the sys-
                         tems under consideration from the point of view
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