This work addresses the problem of designing robust multivariable controllers for the attenuation of the structural response of a helicopter, with reference to the Agusta A109 helicopter. The considered configuration consists of a set of piezoelectric actuators and accelerometers located on the fuselage of the helicopter. The robust harmonic control approach is adopted, based on an data-driven mathematical model of the system.
Robust harmonic control: An application to structural vibration reduction in helicopters
MURA, ROBERTO;PIRODDI, LUIGI;LOVERA, MARCO;GHIRINGHELLI, GIANLUCA
2015-01-01
Abstract
This work addresses the problem of designing robust multivariable controllers for the attenuation of the structural response of a helicopter, with reference to the Agusta A109 helicopter. The considered configuration consists of a set of piezoelectric actuators and accelerometers located on the fuselage of the helicopter. The robust harmonic control approach is adopted, based on an data-driven mathematical model of the system.File in questo prodotto:
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2015 - ACNAAV - DucMuraPiroddiLoveraGhiringhelli.pdf
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