Hybrid electric propulsion systems and methods therefore are provided. More particularly, the present disclosure is directed to control systems for hybrid electric propulsion systems for aerial vehicles that are configured for rapidly and automatically taking action in response to rapid electrical load changes on a torque source, such as an engine. Methods for operating hybrid electric propulsion systems for aerial vehicles are also provided.
Fault Tolerant Hybrid Electric Propulsion System for an Aerial Vehicle
2020-02-27
Patent
Electronic Resource
English
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