Page 270 - Mathematical Models and Algorithms for Power System Optimization
P. 270

262 Chapter 7
                           1
                    0
            When G SðÞ ¼     , a function can be constructed to be similar with the above equation
                         S n +1
                             1
            and equivalent to  , to make:
                            S n
                                              1           1
                                                ¼ lim
                                            S n +1  a!0 ð S + aÞ n +1
            and we have:


                                           1     ∂ n         1
                               0          n                                T
                              G ZðÞ ¼  1ð  Þ  lim    1               1 Z                (7.111)
                                                               Z
                                           n! a!0∂a n   1 e  aT  1
            To sum up, it can be seen that such transformation method must obtain the root of the model
            first, yet the root of the equation with higher order cannot be obtained because there is no
            available direct algorithm. Therefore, it is necessary to use the computer to make the iteration
            solving (such as QR solution) in addition to a great deal of partial methods and combining
            the same terms, the following state equation solution is hereby proposed, without needing any
            iteration solving.


            7.7.3.2 Method of state equation solution

            The first method can be used to solve the problem, but it is not fit for the high-order models of
            multiple roots or three orders or above, and even difficult to program. According to the detailed
            process of the first method, the state equation solution method is conceived in the following
            three steps:

                Step 1: Transform the differential equation into a difference one.
                 1. The differential transfer function G(S) is available.
                    If the transfer function G(S) has been given by the actual engineering system, it must
                    be transformed into differential state equation.
                    In case of

                                                  n
                                        ySðÞ   b 1 S + b 2 S n 1  + ⋯ + b n 1 S + b n
                                  GSðÞ ¼     ¼                                          (7.112)
                                                 n
                                        uSðÞ    S + a 1 S n 1  + ⋯ + a n 1 S + a n
                 it can be transformed into state equation using the following equation:
                 Let:
                                                  X 1 ¼ Y

                 Then:
                                                         _
                                                _
                                           X 2 ¼ Y  d 1 u ¼ X 1  d 1 u
                                                     ⋮
                                                                    _
                            X n ¼ Y n 1   d 1 u n 2   d 2 u n 3   ⋯ d n 1 u ¼ X n 1  d n 1 u  (7.113)
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