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Hysteresis Compensation for a Piezoelectric Actuator of Active Helicopter Rotor Using Compound Control

Active rotor with trailing-edge flaps is a promising method to alleviate vibrations and noise level of helicopters. Hysteresis of the piezoelectric actuators used to drive the flaps can degrade the performance of an active rotor. In this study, bench-top tests are conducted to measure the nonlinear...

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Detalles Bibliográficos
Autores principales: Zhou, Jinlong, Dong, Linghua, Yang, Weidong
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2021
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8621093/
https://www.ncbi.nlm.nih.gov/pubmed/34832710
http://dx.doi.org/10.3390/mi12111298