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Adaptive Dynamic Surface Control of Two-Inertia Systems With LuGre Friction Model  43


                            designs
                                                          δ ie − δ e −z i
                                                             z i
                                                                 i
                                                   S i (z i ) =      .                 (3.16)
                                                            e i + e −z i
                                                             z
                            Then, from (3.16), the transformed error z i is derived as

                                     e i (t)     e i (t)  1   e i (t)    1         e i (t)
                                 −1
                            z i = S        = R i      =   ln      + δ  −   ln δ i −     ,
                                 i                                   i
                                     μ i (t)    μ i (t)  2   μ i (t)     2        μ i (t)
                                                                                        (3.17)
                            where R i (·) is the inverse function of S i (·). The transformed error will be
                            utilized to ensure the prescribed output tracking error performance.

                            3.2.4 High-Gain Tracking Differentiator

                            In this chapter, we will design a control based on DSC. Hence, a filter
                            should be used to avoid the repeated calculation of derivatives of the virtual
                            control signals. To enhance the convergence speed of this operation, high-
                            gain tracking differentiator (HGTD) reported in [30] will be used, which
                            is given by


                                         ϑ 1i (t) = ϑ 2i (t)                           (3.18)
                                         ˙
                                                                 α
                                         ˙
                                         ϑ 2i (t) = H 2    −ρ 1i [ϑ 1 (t) −¯χ i ] − ρ 2i [ϑ 2i (t)/H] β
                            where ρ ji, α, β,and H are positive design parameters, ¯χ i represents the
                            input signal of HGTD, which is the virtual control signals in the DSC
                            design procedure.

                                                                     (j)
                            Lemma 3.2. [30]: If the signal ¯χ i satisfies sup|¯χ | < ∞ for j = 1,2, then the
                                                                     i
                            HGTD (3.18) is convergent for any initial condition within finite-time T > 0,
                            i.e., there exists H > H 0 > 0 and t > T, such that

                                                             a/b
                                                                          ˙
                                         ϑ 1i (t) −¯χ i  è L 1 (1/H) ,  |ϑ 2i (t) − ¯χ i |≤ L 2  (3.19)
                            where L 1,L 2, a, and b are constants.
                               The fast convergence property of HGTD as shown in Lemma 3.2 makes
                            it superior over linear filters in the other DSC control designs to solve the
                            problem of “explosion of complexity” encountered in the backstepping
                            methods.
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