Individual Blade Control Approach for Active Vibration Suppression of a Lift-Offset Coaxial Rotorcraft

This study explores the best vibration reduction using an individual blade control (IBC) actuation scheme for a lift-offset coaxial helicopter in high-speed flight. The rotorcraft dynamics analysis model consists of coaxial, three-bladed counter-rotating rotors and a finite element fuselage stick mo...

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Veröffentlicht in:	Journal of aircraft 2024-07, Vol.61 (4), p.1262-1271
Hauptverfasser:	Hong, Seong Hyun, Kim, Dong Kyun, Jung, Sung Nam
Format:	Artikel
Sprache:	eng
Schlagworte:	Active control Actuation Airframes Flight Helicopter control Individual blade control Rotary wing aircraft Rotating bodies Vibration Vibration analysis Vibration control Vibration measurement
Online-Zugang:	Volltext
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