System and Method for Controlling Rotorcraft

In an embodiment, a rotorcraft includes: a plurality of engines; a flight control computer connected to the plurality of engines, the flight control computer being configured to: receive an operating parameter of a first engine of the plurality of engines; determine an engine output ramping rate for...

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Bibliographische Detailangaben
Hauptverfasser: Ludtke, Christopher James, Alfred, Jillian Samantha, Klein, Morganne Cody
Format: Patent
Sprache:eng
Schlagworte:
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