Partial State Feedback Control with Application to Aircraft Wing Vibration Damping

ISSN： 0022-460X

Source： Journal of Sound and Vibration, Vol.188, Iss.3, 1995-12, pp. : 455-460

Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.

Previous Menu Next

Abstract

Related content

A Neural Network Based Active Vibration Absorber with State Feedback Control

By Ma R.P. Sinha A.

Journal of Sound and Vibration, Vol. 190, Iss. 1, 1996-02 ,pp. : 121-128

Academic Press

Access to resources Recommend Favorite

Vibration Control for the Primary Resonance of a Cantilever Beam by a Time Delay State Feedback

By Maccari A.

Journal of Sound and Vibration, Vol. 259, Iss. 2, 2003-01 ,pp. : 241-251

Academic Press

Access to resources Recommend Favorite

High Damping Capacity Coatings for Surface Vibration Control

Le Journal de Physique IV, Vol. 06, Iss. C8, 1996-12 ,pp. : C8-779-C8-782

Edp Sciences

Access to resources Recommend Favorite

Application of an Efficient Gradient-Based Optimization Strategy for Aircraft Wing Structures

By Dababneh Odeh Kipouros Timoleon Whidborne James F.

Aerospace, Vol. 5, Iss. 1, 2018-01 ,pp. : 3-3

MDPI

Access to resources Recommend Favorite

Multichannel Feedback Control for the Isolation of Base-Excited Vibration

By Serrand M. Elliott S.J.

Journal of Sound and Vibration, Vol. 234, Iss. 4, 2000-07 ,pp. : 681-704

Academic Press

Access to resources Recommend Favorite