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CHAPTER
                                                                   4




                            Neural Network Black Box Modeling of

                            Nonlinear Dynamical Systems: Aircraft

                                                 Controlled Motion







                                                                                 m
                            4.1 ANN MODEL OF AIRCRAFT                  ϕ : R → R as some ANN model with any pre-
                                                                           n
                                    MOTION BASED ON A                  defined accuracy. 1
                                    MULTILAYER NEURAL                    The ANN model design problem for the non-
                                                                       linear controlled dynamical system is treated
                                           NETWORK
                                                                       further as a problem of a neural network ap-
                                                                       proximation of the initial mathematical model
                            As we noted in Chapter 1, many adaptive
                                                                       of the aircraft motion, defined in one way or
                          control schemes require the presence of a con-  another, more often in the form of a system of
                          trolled object model. To obtain such a model,  differential equations. A structural diagram of
                          one needs to solve the classical problem of dy-  the neural network identification process for the
                          namical systems identification [1]. As experience  controlled system that corresponds to this prob-
                          shows, one of the most effective approaches to  lem is presented in Fig. 4.1.
                          solving this problem for nonlinear systems is  The error signal ε that directs the learning of
                          based on the use of ANNs [2–4]. Neural net-  the ANN model is taken to be the squared dif-
                          work modeling allows us to build reasonably  ference between the outputs of the controlled
                                                                       object y p and the neural network model y m for
                          accurate and computationally efficient mod-
                                                                       the control signal u. The trained ANN model im-
                          els.
                                                                       plements a recurrent relation that allows us to
                                                                                                   y
                                                                       compute the value of the output  at time instant
                          4.1.1 The General Structure of the           t i+1 given the values of  y and u at some previous
                                ANN Model of Aircraft Motion           time instants.
                                Based on a Multilayer Neural             We use the Nonlinear Auto-Regressive net-
                                Network                                work with eXternal inputs (NARX) as a model
                                                                       of a dynamical system because it conforms to
                            An ANN is an algorithmically universal math-  the nature of the considered problem of flight
                          ematical model [5–7]. This fact is the basis of
                          the computational efficiency of ANN models. It  1 That is, any nonlinear mapping of the n-dimensional input
                          allows us to represent any nonlinear mapping  vector to the m-dimensional output vector.


                          Neural Network Modeling and Identification of Dynamical Systems
                          https://doi.org/10.1016/B978-0-12-815254-6.00014-9  131       Copyright © 2019 Elsevier Inc. All rights reserved.
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