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Control design and voltage stability analysis of a droop controlled electrical power system for more electric aircraft

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Figure

Fig. 1. Configuration of the studied system in the MEA.
Fig. 3. Control block diagram of the source converter.
Fig. 4), similar to the single source system, the bus voltageIf the system is loaded with CPLs and resistive loads (see Vband total output current Io match the following equation:
Fig. 7. Bode plot of source and load impedances in a system with parallelsources. (a) Overview of source and load impedance
+4

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