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Hybrid Active Vibration Control of Helicopter Fuselage Driven by Piezoelectric Stack Actuators

Research article (Journal of Aircraft, 2018) · cited 25× · AI/ML
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Hybrid Active Vibration Control of Helicopter Fuselage Driven by Piezoelectric Stack Actuators

Summary

Hybrid Active Vibration Control of Helicopter Fuselage Driven by Piezoelectric Stack Actuators is a scholarly article[1].

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  • Hybrid Active Vibration Control of Helicopter Fuselage Driven by Piezoelectric Stack Actuators's instance of is recorded as scholarly article[2].

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Direct Wikidata claims

  1. [2] ↑ . wikidata.org.

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  1. [1] ↑ . Wikidata. wikidata.org.

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APA 4ort.xyz Knowledge Graph. (2026). Hybrid Active Vibration Control of Helicopter Fuselage Driven by Piezoelectric Stack Actuators. Retrieved May 24, 2026, from https://4ort.xyz/entity/hybrid-active-vibration-control-of-helicopter-fuselage-driven-by-piezoelectric-stack-actuators
MLA “Hybrid Active Vibration Control of Helicopter Fuselage Driven by Piezoelectric Stack Actuators.” 4ort.xyz Knowledge Graph, 4ort.xyz, 24 May. 2026, https://4ort.xyz/entity/hybrid-active-vibration-control-of-helicopter-fuselage-driven-by-piezoelectric-stack-actuators.
BibTeX @misc{4ortxyz_hybrid-active-vibration-control-of-helicopter-fuselage-driven-by-piezoelectric-stack-actuators_2026, author = {{4ort.xyz Knowledge Graph}}, title = {{Hybrid Active Vibration Control of Helicopter Fuselage Driven by Piezoelectric Stack Actuators}}, year = {2026}, url = {https://4ort.xyz/entity/hybrid-active-vibration-control-of-helicopter-fuselage-driven-by-piezoelectric-stack-actuators}, note = {Accessed: 2026-05-24}}
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