Non-linear averaged-value models are derived for the twelve-pulse rectifiers that typically form the input stage of more electric aircraft actuator and motor drive systems. Double-wound delta-star and autotransformer configurations are considered. The models allow rectifier and drive system interactions to be examined analytically, or through rapid simulation. The models are validated by comparison with a detailed circuit simulation. (6 pages)
Averaged-value models of twelve-pulse rectifiers for aerospace applications
2004-01-01
Article (Journal)
English
nonlinear averaged-value models , motor drives , rapid simulation , electric actuators , autotransformers , aerospace applications , electric aircraft actuator , twelve-pulse rectifiers , motor drive systems , switching convertors , autotransformer configurations , rectifying circuits , pulse circuits , double-wound delta-star configurations
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