Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
713120 | IFAC-PapersOnLine | 2015 | 6 Pages |
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.
Related Topics
Physical Sciences and Engineering
Engineering
Computational Mechanics