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 and Applied Science > Electronics and Computer Science > Comms, Signal Processing & Control |
| Item ID: | 252517 |
| Date Deposited: | 07 Mar 2004 |
| Last Modified: | 02 Mar 2012 12:19 |
| Contributors: | Aglietti, G S (Author) Langley, R S (Author) Gabriel, S B (Author) Rogers, E (Author) |
| Date: | 1997 |
| Status: | Published |
| Further Information: | Google Scholar |
| URI: | http://eprints.soton.ac.uk/id/eprint/252517 |
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