전자공학회논문지B (Journal of the Korean Institute of Telematics and Electronics B)
- 제33B권3호
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- Pages.193-201
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- 1996
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- 1016-135X(pISSN)
인공위성용 전력시스템 시뮬레이텨 개발
A development of simulator for satellite power system
초록
The space power system for communication satellite which employs the direct energy transfer (DET) method consists of solar array, battry, shunt regulator, charger/discharger and power control unit (PCU). In this paper, the development of the DET power system charger/discharger unit and a microprocessor based PCU is developed for simplicity and flexiblity in the modificatin of control algorithm. A 28V bus voltage, 400W power rting power simulator is built and tested to verify the operation of the simulator at each mode and the stability of mode transition is analyzed.
키워드