Active control of helicopter vibration

J. T. Pearson, R. M. Goodall, I. Lyndon

Research output: Contribution to journalArticle

37 Citations (Scopus)

Abstract

The reduction of helicopter vibration Is of great Importance to the helicopter Industry and considerable effort has been devoted to research into active methods for vibration reduction. This article describes how active control techniques can offer good vibration reduction over significant areas of the fuselage and also provide the capability to adapt to changing speed, rotor conditions and structural dynamics. There are three main areas on the helicopter where active vibration control techniques can be applied: at the rotor, at the main gearbox to fuselage interface, and within the fuselage itself. The last area is termed the active control of structural response (ACSR) and is considered In more detail. Finally, the performance of the ACSR technique in minimising vibration in helicopter structures Is analysed using results which demonstrate the performance potential under differing conditions.

LanguageEnglish
Pages277-284
Number of pages8
JournalComputing and Control Engineering Journal
Volume5
Issue number6
DOIs
Publication statusPublished - 1 Dec 1994
Externally publishedYes

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Helicopters
Fuselages
Rotors
Structural dynamics
Vibration control
Industry

Cite this

Pearson, J. T. ; Goodall, R. M. ; Lyndon, I. / Active control of helicopter vibration. In: Computing and Control Engineering Journal. 1994 ; Vol. 5, No. 6. pp. 277-284.
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Active control of helicopter vibration. / Pearson, J. T.; Goodall, R. M.; Lyndon, I.

In: Computing and Control Engineering Journal, Vol. 5, No. 6, 01.12.1994, p. 277-284.

Research output: Contribution to journalArticle

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