SYSTEM AND METHOD FOR CONTROLLING ROTORCRAFT

In an embodiment, a rotorcraft (101) includes: a rotor system (103); a sensor (207); a flight control device; and a flight control computer (FCC) (205) coupled to the rotor system (103), the sensor (207), and the flight control device, the FCC (205) configured to: determine a rotation speed of the r...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	ALFRED, Jillian Samantha, BOTHWELL, Christopher M
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	CONTROLLING PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
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Beschreibung
Zusammenfassung:	In an embodiment, a rotorcraft (101) includes: a rotor system (103); a sensor (207); a flight control device; and a flight control computer (FCC) (205) coupled to the rotor system (103), the sensor (207), and the flight control device, the FCC (205) configured to: determine a rotation speed of the rotor system (103); select a first aeroservoelasticity filter configuration from a plurality of aeroservoelasticity filter configurations according to the rotation speed of the rotor system (103), the aeroservoelasticity filter configurations being predetermined configurations corresponding to different rotation speeds of the rotor system (103); receive a signal from the sensor (207); filter the signal according to the first aeroservoelasticity filter configuration; and adjust the flight control device according to the filtered signal.