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Author Mura, R. ♦ Lovera, M.
Source IEEE Xplore Digital Library
Content type Text
Publisher Institute of Electrical and Electronics Engineers, Inc. (IEEE)
File Format PDF
Copyright Year ©2014
Language English
Subject Domain (in DDC) Technology ♦ Engineering & allied operations ♦ Other branches of engineering
Subject Keyword Rotors ♦ Robustness ♦ Vibrations ♦ Uncertainty ♦ Helicopters ♦ Actuators ♦ Vectors
Abstract In this paper a novel approach to the design of active controllers aimed at reducing vibrations in helicopter applications is proposed. In particular the role of variability in the vibratory response of the helicopter (such as due to, e.g., varying flight condition and actuator nonlinearities) is taken into account in the synthesis of a robust parameter-varying controller, based on a discrete-time LPV model of the system. Numerical examples demonstrate the effectiveness of the proposed approach, in comparison to other classical strategies.
Description Author affiliation: Dipt. di Elettron., Politec. di Milano, Milan, Italy (Mura, R.; Lovera, M.)
ISBN 9781479974092
Educational Role Student ♦ Teacher
Age Range above 22 year
Educational Use Research ♦ Reading
Education Level UG and PG
Learning Resource Type Article
Publisher Date 2014-10-08
Publisher Place France
Rights Holder Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Size (in Bytes) 831.79 kB
Page Count 6
Starting Page 427
Ending Page 432

Source: IEEE Xplore Digital Library