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APPC of Strict-Feedback Systems With Non-linear Dead-Zone  169


                            Integrating (10.51)over [0,t],itcan be obtained

                                         c
                                                                  c
                                      n                        n
                                ϑ +   i=1 i1M i /2       ϑ +   i=1 i1M i /2  −γt
                            V ≤                + V(0) −                   e
                                       γ                        γ
                                             t
                                        n

                                                                γς
                                                              ˙
                                + e −γt       α[G i (x)N(ξ i ) + 1]ξ ie dς
                                         i=1
                                            0
                                      n                                t
                                         c
                                ϑ +   i=1 i1M i /2     −γt  −γt    n                     γς
                                                                                       ˙
                              ≤                + V(0)e   + e           α[G i (x)N(ξ i ) + 1]ξ ie dς
                                       γ                          i=1  0
                                                                                      (10.52)
                            Consequently, one can rewrite (10.52)as
                                                         t
                                                   n
                                                                           γς
                                                                         ˙
                                    V(t) ≤ δ + e −γt     α[G i (x)N(ξ i ) + 1]ξ ie dς  (10.53)
                                                    i=1
                                                       0
                                             n
                                                c
                            where δ = ϑ +    i=1 i1M i /2 /γ + V(0) is a positive constant. Then
                            according to Lemma 10.2, it can be concluded that V i, ξ i ,and
                               t        ˙ γς                                            ∗  ∗
                             0  G i (x)N(ξ i )ξ ie dς are all bounded on [0,t f ). In addition, since θ , ε ,
                                                                                        i
                                                                                           i
                            and y d , ˙y d are all bounded, ˆ , ˆε i, ˙ ,and x i, z i are then bounded, which
                                                          ξ i
                                                    θ i
                            further implies that the control signals α i and v are bounded. According to
                            Proposition 2 in [28], if the solution of the closed-loop system is bounded
                            on the interval [0,t f ) for any t f > 0, it is also true as t f →∞ as discussed
                            in [13,28]. Consequently, we get that all signals in the control system are
                            bounded. Moreover, as stated in Lemma 10.1, the boundedness of z 1 is
                            sufficient to guarantee the PPF condition (10.4)via theproposederror
                            transformation. This means that the tracking control of system (10.1)with
                            guaranteed performance (10.4)isachieved.
                               It should be noted that the estimated vector ˆ W i is replaced by a scalar
                                                                              ∗
                                                                    ∗
                            θ i through introducing an unknown scalar θ = W ∗T W as the adaptive
                            ˆ
                                                                   i     i   i
                            parameter of HONN, such that the computational cost of the proposed
                            control can be reduced significantly. Moreover, with the help of Nussbaum-
                            type function, the unknown signs of g i (¯x i ) and unknown dead-zone non-
                            linearity are all handled. The functions k ij (·) and parameters g 0i, g 1i are not
                            used in the control implementation.
                            10.4 SIMULATIONS
                            To illustrate the validity of the proposed control, consider the following
                            non-linear time-delay system
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