Initial modelling and controller design for active control of spacecraft microvibrations
Initial modelling and controller design for active control of spacecraft microvibrations
633-640
Aglietti, G.S.
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Gabriel, S.B.
ac76976d-74fd-40a0-808d-c9f68a38f259
Langley, R.S.
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Rogers, E.
611b1de0-c505-472e-a03f-c5294c63bb72
1996
Aglietti, G.S.
e44d0dd4-0f71-4399-93d2-b802365cfb9e
Gabriel, S.B.
ac76976d-74fd-40a0-808d-c9f68a38f259
Langley, R.S.
3fac905f-197c-45b4-bd7c-c2df2235e279
Rogers, E.
611b1de0-c505-472e-a03f-c5294c63bb72
Aglietti, G.S., Gabriel, S.B., Langley, R.S. and Rogers, E.
(1996)
Initial modelling and controller design for active control of spacecraft microvibrations.
Burke, W.R.
(ed.)
In Proceedings of the European Space Agency Conference on Spacecraft Structures, Materials, and Mechanical Testing.
European Space Agency.
.
Record type:
Conference or Workshop Item
(Paper)
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More information
Published date: 1996
Venue - Dates:
The European Space Agency (ESA) Conference on Spacecraft Structures, Materials and Mechanical Testing, Noordwijk, The Netherlands, 1996-03-27 - 1996-03-29
Identifiers
Local EPrints ID: 22208
URI: http://eprints.soton.ac.uk/id/eprint/22208
PURE UUID: c72b75aa-7cf6-4676-82bd-6374cd159bfc
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Date deposited: 14 Feb 2007
Last modified: 18 Jan 2024 02:33
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Contributors
Author:
G.S. Aglietti
Author:
S.B. Gabriel
Author:
R.S. Langley
Author:
E. Rogers
Editor:
W.R. Burke
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