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Multi-level integrated optimal design for power systems of more electric aircraft

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Academic year: 2021

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Figure

Fig. 1. Trend in commercial aircraft power demand. Table 1
Fig. 2. Actuation system architecture.
Fig. 3. Flight mission in the HSPMSM torque-speed plane.
Fig. 5. Typical plots of electrical variables at the filter input and output. (a) Input and output voltages
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