I. Introduction
Due to the mature structure, high reliability, and low maintenance, the brushless synchronous machine (BSM) is still the most attractive candidate generator topology for both fixed-frequency and variable-frequency ac power generation for civil aircraft. It also has the potential to be used as the starter for engine cranking [1]–[3]. In the generation mode, the ac output of the main exciter of BSM is rectified by a rotating rectifier and employed for the dc excitation of main generator. The output voltage magnitude can then be regulated through an automatic voltage regulator to compensate for the variable speed and changing load. However, in the starting mode, the main exciter cannot offer excitation power for the main generator from standstill to the low speed range by the conventional dc excitation method. Thus, excitation becomes the first key issue of BSM used as starter in variable frequency ac power system [4].