2022
DOI: 10.1007/s42405-022-00440-z
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Multicyclic Vibration Control of a Helicopter Rotor with Active Twist Actuation

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Cited by 6 publications
(2 citation statements)
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“…The rotor system imbalance creates an excitation force, and the response can be measured by accelerometers and tachometers. In the case of known fuselage response and system parameters, vibration analysis is to screen the system input signal to achieve the purpose of discriminating environmental characteristics [8].…”
Section: Vibration Analysismentioning
confidence: 99%
“…The rotor system imbalance creates an excitation force, and the response can be measured by accelerometers and tachometers. In the case of known fuselage response and system parameters, vibration analysis is to screen the system input signal to achieve the purpose of discriminating environmental characteristics [8].…”
Section: Vibration Analysismentioning
confidence: 99%
“…[40], directly derives from the capability of reducing the power consumption and optimizing the load distribution on the blade; • Abatement of noise and vibrations up to 65%, as discussed in refs. [41,42]; • Enhancement of the safety and stability of the rotorcraft in case of failure and gust. This aspect is strictly related to the better distribution of the loads on the blade, obtainable by altering the twist, and to the mitigation of vibration at the hub.…”
mentioning
confidence: 99%