Adaptation and control of a latching current limiter based on a SiC N-MOSFET
Palabra(s) clave:
LCL
SiC N-MOS
wide bandgap devices
current protection
Fecha de publicación:
Resumen:
Latching current limiters (LCLs) are circuits used for electrical load control on spacecrafts. They provide enhanced over current protection, improving reliability. LCL classic implementations are based on the use P-MOSFETs as the main current limiting device. However, new wide bandgap materials (WBG) offer the possibility to operate at higher voltages and, allegedly higher temperatures. Therefore, it exists the possibility to design an LCL architecture based on a SiC N-MOS device. In order to control the LCL and to adapt its working behaviour to a different N-MOS, the most important stages are the analog isolator (DCX) which is the one that controls the gate-source voltage level of the N-MOS, and the current control loop in charge of react if the sensed current is higher or not regarding the current reference. This way, this work presents a guideline for the design of the DCX and the current control loop stages. Finally, some experimental results for a class 10 LCL, following the proposed designs, for a bus voltage of 100 V will be shown.
Latching current limiters (LCLs) are circuits used for electrical load control on spacecrafts. They provide enhanced over current protection, improving reliability. LCL classic implementations are based on the use P-MOSFETs as the main current limiting device. However, new wide bandgap materials (WBG) offer the possibility to operate at higher voltages and, allegedly higher temperatures. Therefore, it exists the possibility to design an LCL architecture based on a SiC N-MOS device. In order to control the LCL and to adapt its working behaviour to a different N-MOS, the most important stages are the analog isolator (DCX) which is the one that controls the gate-source voltage level of the N-MOS, and the current control loop in charge of react if the sensed current is higher or not regarding the current reference. This way, this work presents a guideline for the design of the DCX and the current control loop stages. Finally, some experimental results for a class 10 LCL, following the proposed designs, for a bus voltage of 100 V will be shown.
Descripción:
European Space Power Conference, ESPC 2023 (13th. 2023. Elche, Spain)
Patrocinado por:
This work has been carried out by funding from the Spanish government through the PID2021-127707OB-C21 project, and the PRE2019-088425 grant. In the same way, this work has been supported by the Principality of Asturias and FICYT under the SV-PA-21-AYUD/2021/51931 project.