The thesis focuses on the development and testing of a test board for the STGAP4S gate driver and confirms its suitability for the efficient control of SiC MOS transistors in the inverter of the electric propulsion system of the Pipistrel Nuuva V300 unmanned aircraft.
In the theoretical part, synchronous electric motors and inverters powered by SiC MOS transistors are presented. The structure and operation of both conventional silicon MOS transistors and more advanced SiC MOS transistors are described. The SiC module CAB425M12XM3, used in the inverter application of the Nuuva V300, is explained in more detail. The operation of flyback converters and SPI communication is also discussed. The STGAP4S gate driver is analyzed and described, including its integrated protection features, as well as the embedded flyback controller. The circuit development process is presented, from schematic design to printed circuit board fabrication. Finally, measurements and their results are shown.
The development board with the STGAP4S driver was successfully developed and tested. Measurement results showed that the STGAP4S can provide the necessary voltage levels for switching SiC MOS transistors while delivering the required currents for switching times within 0.5 μs. The STGAP4S driver proved to be suitable for use in the Nuuva V300 inverter.
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