Influence of flexible interface on the performance of whole spacecraft vibration isolation

ISSN： 0002-2667

Source： Aircraft Engineering, Vol.80, Iss.1, 2008-01, pp. : 35-43

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

Maneuvers and vibration suppression of flexible spacecraft with input nonlinearities

By Hu Qinglei Ma Guangfu

Aircraft Engineering, Vol. 77, Iss. 5, 2005-05 ,pp. : 388-400

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Active Vibration Isolation of Helicopter Rotors

By Smollen Leonard E. Marshall Philip Gabel Richard

Journal of the American Helicopter Society, Vol. 7, Iss. 2, 1962-04 ,pp. : 42-55

AHS International

Access to resources Recommend Favorite

Antiresonant Rotor Isolation for Vibration Reduction

By Desjardins Rene A. Hooper W. E.

Journal of the American Helicopter Society, Vol. 25, Iss. 3, 1980-07 ,pp. : 46-55

AHS International

Access to resources Recommend Favorite

Spacecraft vibration reduction using pulse modulated command input and smart materials

By Hu Qinglei

Aircraft Engineering, Vol. 78, Iss. 5, 2006-09 ,pp. : 378-386

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Dynamics of vibration isolation system obeying fractional differentiation

By Li Song Fang Bo Yang Tianzhi Zhang Yewei Tan Lijun Huang Wenhu

Aircraft Engineering, Vol. 84, Iss. 2, 2012-03 ,pp. : 103-108

Emerald Group Publishing Ltd

Access to resources Recommend Favorite