Permanent magnet assisted reluctance (PMAREL) machine possesses the potential as the aircraft starter/generator (S/G) for its high power density, high efficiency and tolerance to short-circuit faults. For aircraft S/G systems, the voltage build-up is a prerequisite for power generation. However, the voltage build-up of the PMAREL S/G system may fail if the initial DC-link voltage is low and the control is fast-response. In this paper, the mechanism of the voltage build-up failure is clarified. The conduction feature of power devices in the power electronic converter when the DC-link voltage is clamped at 0 V are explored. Conditions for clamping the DC-link voltage at 0 V all the time is determined. An integrated control method is proposed to cope with the voltage build-up failure as well as improve the dynamic performance of the S/G system. Based on a prototype of PMAREL S/G system, the correctness of the analysis and the effectiveness of the proposed method are verified through experiments.
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