New control technique based on the LAC/HAC concept for flexible structures

Shinji Hokamoto, Norihiro Goto

Research output: Contribution to journalArticle

1 Citation (Scopus)

Abstract

In this paper a new control technique based on the LAC/HAC concept is proposed to suppress the vibration of flexible space structures. The new technique employs the mechanism to turn on or off the HAC part of the LAC/HAC system in such a manner as to suppress the spillover effects as quickly as possible. The control system designed by the new technique has global stability and is more effective than a pure LAC system, even when an ordinary LAC/HAC system results in failure because of spillover instability. To show the characteristic features of the new technique and how to implement the system, computer simulation examples are given. Finally, the technique is applied to the transversal vibration control of a cantilever beam to show its effectiveness and practicality.

Original languageEnglish
Pages (from-to)240-249
Number of pages10
JournalTransactions of the Japan Society for Aeronautical and Space Sciences
Volume34
Issue number106
Publication statusPublished - Feb 1 1992
Externally publishedYes

Fingerprint

Flexible structures
vibration
spillover effect
computer systems simulation
Cantilever beams
Vibration control
computer simulation
control system
cantilever beams
Control systems
Computer simulation

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Space and Planetary Science

Cite this

New control technique based on the LAC/HAC concept for flexible structures. / Hokamoto, Shinji; Goto, Norihiro.

In: Transactions of the Japan Society for Aeronautical and Space Sciences, Vol. 34, No. 106, 01.02.1992, p. 240-249.

Research output: Contribution to journalArticle

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