作者: S. J. Forrest , J. Wang , G. W. Jewell , C. M. Johnson , S.D. Calverley
DOI: 10.1109/IPEMC.2006.4778138
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摘要: This paper proposes an N-phase, AC fed, switched reluctance drive for aerospace applications. The proposed converter is capable of direct conversion and eliminates the unreliable DC link capacitor present in conventional supply converters. It shown that, by Space Vector Modulation output current, control active reactive power can be achieved whilst three sinusoidal input phase-currents with required factor synthesised. A comparison between numerically simulated analytically predicted current ripple also presented.