A Modelling Technique for Active Control Design Studies with Application to Spacecraft Microvibrations


Aglietti, G S, Langley, R S, Gabriel, S B and Rogers, E (1997) A Modelling Technique for Active Control Design Studies with Application to Spacecraft Microvibrations. Journal of The Acoustical Society of America, 102, (4), 2158-2166.

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Item Type: Article
Divisions: Faculty of Physical Sciences and Engineering > Electronics and Computer Science > Comms, Signal Processing & Control
ePrint ID: 252517
Date Deposited: 07 Mar 2004
Last Modified: 27 Mar 2014 19:54
Further Information:Google Scholar
URI: http://eprints.soton.ac.uk/id/eprint/252517

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