2016
DOI: 10.1177/1077546316655707
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Hybrid active suspension system of a helicopter main gearbox

Abstract: This paper considers experiments on the control of a helicopter gearbox hybrid electromagnetic suspension. As the new generation of helicopters includes variable engine revolutions per minute (RPMs) during flight, it becomes relevant to add active control to their suspension systems. Most active system performance derives directly from the controller construction, its optimization to the system controlled, and the disturbances expected. An investigation on a feedback and feedforward filtered-x least mean squar… Show more

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Cited by 12 publications
(11 citation statements)
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“…In [83,84] an active suspension system is developed to enhance the performances of the dynamic antiresonant vibration absorber traditionally employed in helicopters [85]. In particular, the main advantage of the passive absorber combined with an active part is the power reduction.…”
Section: Antiresonance Assignment In Helicoptersmentioning
confidence: 99%
“…In [83,84] an active suspension system is developed to enhance the performances of the dynamic antiresonant vibration absorber traditionally employed in helicopters [85]. In particular, the main advantage of the passive absorber combined with an active part is the power reduction.…”
Section: Antiresonance Assignment In Helicoptersmentioning
confidence: 99%
“…Semi-active control has been favored by researchers in recent years for its advantages of low power consumption, high reliability, and comparable to active control. Based on SARIB, Rodriguez et al (2018) controlled the relative rotational movement of the flapper arm with a voice coil actuator, and feedforward filtered-x least mean square control were applied to create a semi-active suspension with larger bandwidth efficiency, which were successfully achieved by simulations and experiments. Scheidler et al (2016) designed a magnetostrictive spring with dynamically adjustable rigidity, which can change the natural frequency to adapt to the change of source frequency.…”
Section: Introductionmentioning
confidence: 99%
“…the damper will work as a tuned mass damper when the controller is turned off [29]. Systems have been proposed such as an HMD with H∞ optimum parameters to minimize both response and control effort [30], a fail-safe system [31], a dual loop approach to increase stability margins [32], an FXLMS controller with a resonant isolation system (SARIB) for helicopter applications [33], delay resonators [34], a tunable vibration absorber [35], an adaptive inertial mass device [36] and an hyperstable HMD [25,37].…”
Section: Introductionmentioning
confidence: 99%