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148                                 Modern Control of DC-Based Power Systems


             The Kalman filter estimates the state of a plant based on the input sig-
          nals and measurements. However, the plant is not just driven by a known
          control signal uðtÞ but also by an unknown plant noise wðtÞ. Furthermore,
          the measurements yðtÞ include a noise signal vtðÞ which is called measure-
          ment noise. This leads to the following continuous linear time invariant
          plant model:


                              _ x tðÞ 5 Ax tðÞ 1 Bu tðÞ 1 Fw tðÞ
                                                                      (5.97)
                                  ytðÞ 5 Cx tðÞ 1 HvðtÞ
             Typically, the noise signals are assumed to be uncorrelated white
          Gaussian noise with zero mean and the following covariance matrices S w
          and S v .
             For an infinite time horizon the optimal state estimation problem can
          be formulated such that the cost J of the mean square estimation error is
          minimized:
                               T
                           8                                 9
                              1
                           <   ð                             =
                                              T
                 J 5 lim E        ð x tðÞ 2 ~x tðÞÞC Cðx tðÞ 2 ~x tðÞ dt  (5.98)
                             T
                     T-N :                                   ;
                               0
             Where E .. . is the expected value. Under the assumption that CA is
          observable the solution of (5.99) applied to the system of (5.98) will lead
          to the Kalman filter [33]. The structure of the Kalman filter can be
          depicted in various forms of which one of them is the predictor/corrector
          form [45]:
                          _                                           (5.99)
                          ^ x tðÞ 5 A^x tðÞ 1 ButðÞ 1 K½ytðÞ 2 C^xðtފ
             This terminology appeared first for discrete Kalman filters. It describes
          how the derivative of the estimation is first predicted from old data and
          then updated using new measurements [33]. Eq. (5.99) clarifies that the
          only unknown variable is the Kalman gain K, which is calculated as
          follows:
                                        T    21  T 21
                                             v
                                K 5 PC ðHS H Þ                       (5.100)
             Since the time-varying solution of the differential equation is close to
          the steady-state solution when the system is running for a long time, the
          derivatives in the Riccati equation are set to zero and where P is the
          solution of the algebraic Riccati Eq. (5.101):

                                                         T
                                          T 21
                                 T
                        T
                                      21
                 AP 1 A P 2 PC ðHS H Þ CP 1 FS w F 5 0               (5.101)
                                      v
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