Page 141 - Modern Control of DC-Based Power Systems
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Generation Side Control                                      105


                 For the implementation of the DC DC conversion stage, various
              technologies could be used, e.g., buck converter, DAB, or MMC. The
              buck converter is selected, considering that unidirectional power flow is
              necessary.
                 Van der Broeck et al. stated about buck converters [6]:
             •  They provide a low-cost and robust topology, exhibit well known
                steady state and dynamic properties and the design procedures for
                these converters have been studied intensively.
             •  However, the control of a one quadrant buck converter over a wide
                load range and varying voltage transfer ratios is challenging.







                   4.2 STATE-SPACE MODEL
                   The modeling of the ISPS in this book is based on Ref. [7], which
              is a radial concept topology. It features a DC bus and the loads are con-
              nected either through a DC DC converter, which throughout this book
              has been referred to as a point of load converter directly bus or via a load
              zone. The generation devices are connected via a rectifier and a following
              DC DC converter to the MVDC bus, this DC DC converter will be
              abbreviated as line regulating converter (LRC). A more detailed represen-
              tation is depicted in Fig. 4.2 [8]. It will be presumed that each load zone
              can be represented by a lumped load.
                 In the model, four generating systems (G1 G4) are considered, which
              are connected through rectifiers (C1 C4) in cascade with buck conver-
              ters, i.e., LRC (C5 C8) to the MVDC bus. The MVDC bus feeds all the
              shipboard loads, through service power converters (C9 C15). In Fig. 4.2
              the loads M1 and M2 are ship propulsion motors, each fed by inverters.
              The loads and propulsion motors are connected to the MVDC bus
              through cables (CA1 CA6). Loads L2 and L3 are LVDC (low voltage
              DC utility) and LVAC (low voltage AC utility) loads and are respectively
              fed by buck converters and inverters. It has to be highlighted that the stor-
              age components which are mentioned in Ref. [7], such as supercapacitor,
              batteries, or flywheel, are omitted from the analysis in this book.
                 From Fig. 4.2 the general circuit model representation of the system
              can be derived. It is depicted in Fig. 4.3. The representation shows n DC
              generating systems in parallel with m loads. In this circuit model the DC
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