Show simple item record

contributor authorJ. T. Sawicki
contributor authorW. K. Gawronski
date accessioned2017-05-08T23:53:30Z
date available2017-05-08T23:53:30Z
date copyrightApril, 1997
date issued1997
identifier issn1528-8919
identifier otherJETPEZ-26764#456_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/118705
description abstractAn effective technique is applied to the suppression of vibrations in flexible rotor-bearing systems with small gyroscopic effects. A balanced linear-quadratic-Gaussian (LQG) controller design procedure is implemented. The size of the controller is reduced in two stages by using (i) a balanced model reduction, and (ii) an LQG balanced reduction. The condition for a gyroscopic matrix is developed that allows one to ignore the rotor gyroscopic effects in the process of the controller design, although they are included in the rotor dynamics. The approach is illustrated on a typical rotor-bearing system represented by a 48 degree-of-freedom finite element model.
publisherThe American Society of Mechanical Engineers (ASME)
titleBalanced Model Reduction and Control of Rotor-Bearing Systems
typeJournal Paper
journal volume119
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2815596
journal fristpage456
journal lastpage463
identifier eissn0742-4795
keywordsBearings
keywordsRotors
keywordsControl equipment
keywordsDesign
keywordsRotordynamics
keywordsDegrees of freedom
keywordsVibration AND Finite element model
treeJournal of Engineering for Gas Turbines and Power:;1997:;volume( 119 ):;issue: 002
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record