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Control Approaches for Parallel Source Converter Systems     155


                 The system would be stable if there were no modeling errors or dis-
              turbances are present and the virtual disturbance estimate is perfect. This
              would mean that the set-point trajectory generator alone could output
              the control signal which drives the system to its equilibrium point.
                 Since in real applications this is not the case, an additional LQR con-
              troller is added for optimal state feedback. The goal of this control strat-
              egy is the minimization of a cost function that includes the states as well
              as the control signal. By assuming that the controller will operate for a
              longer period than the transient time of the optimal gains [50], the LQG
              controller is supposed to minimize the cost function for an infinite time
              interval.
                 The steady-state solution of the following cost function (J i Þ has to be
              found:

                                  ð N
                                    	            2          2
                           J i 5 E   Q V 2V nom Þ 1 R d2d e Þ  dt       (5.119)
                                       y
                                                      ð
                                        ð
                                  0
                 Eq. (5.119) can be transformed into the general cost function form in
              [33]:
                          ð N
                            	      T                  T
                   J 5 E     ð x2x e Þ Qx 2 x e Þ 1 d2d e Þ R d 2 d e Þ dt  (5.120)
                                                ð
                                                        ð
                                      ð
                          0
                              T
                 Where Q 5 C QC is a symmetric, positive-semidefinite weighting
              matrix and R becomes a positive weighting scalar.
                 By using the feedback gain matrix of the LQR on the state estimates
              of the Kalman filter a state feedback which minimizes the optimization
              problem can be obtained:
                                          21
                                             T
                                   d 52 R B Px 52 K ^x                  (5.121)
                 P is found from the steady-state solution of the Riccati differential
              equation which satisfies the algebraic Riccati equation:

                                               21 T
                                     T
                              PA 1 A P 2 PBR B P 1 Q 5 0                (5.122)

              5.4.2.2 Augmented Local Kalman Filter
              The design will be performed in two consecutive steps. First, the distur-
              bance I d in the system is simply included as noise rather than as a state
              and the Kalman filter is introduced to estimate the inductor current of
              the buck converter. Second, this Kalman filter is augmented to include
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