Current regulation of permanent magnet excited synchronous motors for guided missiles involves deriving current vector, magnitude/angle corrections from measurement currents

摘要

The current regulation method involves deriving the magnitude of the current vector from two measurement current components (I1M,I2M ) by taking the square root of the sum of the squares and deriving correction values for the magnitude and angle terms, which are added to the demanded value for the magnitude and angle in correction regulators.