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116    3. NEURAL NETWORK BLACK BOX APPROACH TO THE MODELING AND CONTROL OF DYNAMICAL SYSTEMS


































                         FIGURE 3.14 The results of testing the neurocontroller combined with the neural network model of the controlled object.
                         The solid line is the output of the model (3.25); the dotted line is the output of the neural network model; V z is the component
                         of the velocity vector along the Oz-axis; q is the angular velocity of the pitch; θ is angle of pitch; δ e is the deflection angle
                                                                        (ref )      (ref )
                         of the stabilizer; t is the time; EV y , Eq are the differences |V z − V z  | and |q − q  |, respectively (From [99], used with
                         permission from Moscow Aviation Institute).

                            Assuming the norms of the vectors ||x|| and  the choice of the operation mode of the dynam-
                         ||u|| to be small, we can get the linearized equa-  ical system, i.e., source of its multimode behav-
                         tions of the disturbed motion of the object (3.28),  ior. We need to clarify the nature of the uncer-
                                                                      tainty introduced by the vector λ ∈  .Later,in
                                         ˙ x = Ax + Bu,        (3.31)
                                                                      the synthesis of the neurocontroller, this vector
                         in which the elements of matrices A and B are  is assumed to be completely observable. How-
                         functions of the parameters of program motion  ever, during the synthesis process, we have no
                                                  s
                         (3.29), elements λ ∈   ⊂ R , and, possibly, the  a priori data on the values of λ for each of the
                         time t, i.e.,                                instants of time t 0   t i   t f . These values be-
                                                                      come known only at the moment t i ,forwhich
                                                0
                                                   0
                                   ||a ij || = ||a i,j (  x ,  u ,λ,t)||,
                                                                      the corresponding control u(t i ) must be gener-
                                                0
                                                   0
                                   ||b ik || = ||b i,k (  x ,  u ,λ,t)||,  ated.
                                     i,j ∈{1,...,n},                     We assume that the system under consider-
                                                                      ation consists of a controlled object (plant), a
                                       k ∈{1,...,m},
                                                                      command device (controller) producing control
                            In the problem under consideration, it is the  signals, and an actuator system generating con-
                         vector λ ∈   that is the source of uncertainty in  trol actions for a given control signal.
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