Systems and methods for controlling aircraft electrical power

Systems and methods for controlling aircraft electrical power are disclosed. A system in accordance with one embodiment includes an electric motor, an aircraft load coupled to the electric motor and powered by the electric motor, and a motor controller coupled to the electric motor to vary an output...

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Bibliographische Detailangaben

Hauptverfasser:	White, Jeffrey J, Toy, David K, Groat, J. Everett
Format:	Patent
Sprache:	eng
Online-Zugang:	Volltext bestellen
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