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This paper proposes a comprehensive simulation model for the Electrical Power System (EPS) of More Electrical Aircrafts (MEA). Taking the presently typical MEA model of Boeing 787 as an example, the integrated structure of EPS is firstly illustrated and the operating principles are theorized. The key components of the MEA EPS including generators, rectifiers, loads, breakers, control devices, cables...
This article introduces the operation principle of the four-quadrant rectifier. It expounds the design of the system and control circuits that bases on STM32 and four-quadrant rectifier. The simulation result showed that performance of the system is perfect. And the application of STM32 completed the design of control system, and validated by experiment, showing that the system can realize four quadrant...
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