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Speed Closed-Loop Control of Permanent Magnet Synchronous Motor for All-Electric Aircraft Applications Based on Active Disturbance Rejection Controller |
Cui Shumei1, Kuang Zhi1, Du Bochao1, Ostanin Sergei Yurievich2, Milyaev Igor Matveevich3 |
1. School of Electrical Engineering and Automation Harbin Institute of Technology Harbin 150001 China; 2. Moscow Power Engineering Institute Moscow 111250 Russia; 3. A.A. Baikov Institute of Metallurgy and Material Science Yekaterinburg 620016 Russia |
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Abstract This paper utilized permanent magnet synchronous motor (PMSM) to directly drive the propeller blade of an electric aircraft, in order to restrain unstable air flow effects for output torque and improve disturbance rejection ability for propeller, speed closed loop control of PMSM based on active disturbance rejection controller (ADRC) was employed. The torque requirement on propeller blade operation was analyzed in different flying status, the model of speed closed loop based on ADRC was built and the flying condition was simulated by using Dspace. The simulation and experiment results validate the ability to resist load disturbance, the response of speed is stable and the output torque accord with required torque for propeller during the whole flying statues.
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Received: 20 August 2016
Published: 14 September 2017
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