Abstract
The increase of electrical drives power density and reliability allows the possibility to develop an all-electric propulsion systems for the aircraft. A configuration based on a mono-inverter dual-parallel (MIDP) permanent magnet synchronous motors could be suitable in order to reduce the cost and the weight of the propulsion systems. This paper proposes a novel current references limitation strategy to improve the overall dynamic behaviour of the system during transient operations, without the worsening of oscillations damping. The effectiveness of the proposed solution is demonstrated through numerical simulations.
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