대한전기학회논문지:전기기기및에너지변환시스템부문B (The Transactions of the Korean Institute of Electrical Engineers B)

대한전기학회 (The Korean Institute of Electrical Engineers)
권호 표지

전력회수 능력을 갖는 전압원 컨버터-인버터 세트로 구성 된 부하모의 장치

Load Simulator with Power-Recovery Capability Based on Voltage Source Converter-Inverter Set

  • 발행 : 2005.04.01
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초록

This paper describes a load simulator with power-recovery capability, which is based on the voltage source converter-inverter set. The load simulator described in this paper can save the electric energy that should be consumed to test the operation and performance of the distributed generation system and the power quality compensator. The load simulator consists of a converter-inverter set with a DSP controller for system control and PWM pulse generation. The converter operates as a universal load to model the linear load and the non-linear load, while the inverter feed the energy back to the power source with harmonic compensation. The load simulator can be widely used in the lab to test the performance of the distributed generation system and the power quality compensator.

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참고문헌

  1. H. Akagi, Y. Kanazawa and A. Nabae, 'Generalized Theory of the Instantaneous Reactive Power in Three-Phase Circuits' Int. Conf. Power Electronics, Tokyo, 1983, pp. 1375-1386
  2. Malesani, L., Rossetto, L., and Tenti, P, 'Active Filter for reactive power and harmonics compensation', IEEE Power Electron. Spec. Conf. Rec., pp. 321-330, 1996
  3. L. Moran, P. Godoy, R. Wallace, J.Dixon, 'A New Current Control Strategy for Active Power Filters Using Three PWM Voltage Source Inverters', IEEE, PESC, pp. 3-9, 1993 https://doi.org/10.1109/PESC.1993.471930
  4. Ando, I, Takahashi. I, Tanaka. Y, Ikehara. M, ' Electric load controlled by computer simulator having power regeneration ability', IEEE Power Conversion Conf, vol. 2, pp. 9225-930, 1997 https://doi.org/10.1109/PCCON.1997.638377
  5. Guan-Chyun Hsieh, Jung-Chien Li, ' Design and implementation of an AC active load simulator circuit ', IEEE Trans. Aerospace and Electronic Systems, vol 29, pp. 157-165, 1993 https://doi.org/10.1109/7.249121