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dc.contributor.authorGleave, J.
dc.contributor.authorAgrawal, B.N.
dc.dateMarch 1998
dc.date.accessioned2013-07-18T19:18:27Z
dc.date.available2013-07-18T19:18:27Z
dc.date.issued1998
dc.identifier.citationIEEE proceedings: Aerospace Conference, Snowmass, CO, March 1998.
dc.identifier.urihttp://hdl.handle.net/10945/34534
dc.descriptionThe article of record as published may be found at http://dx.doi.org/10.1109/AERO.1998.686819en_US
dc.description.abstractFor spacecraft with large flexible antennas, and or flexible support structures, suppressing vibrations caused by on-orbit operational disturbances (e.g., antenna slew maneuvers and thruster firings) is a challenging problem. In the past several years, advances in smart structure technologies have made their use in real-time dynamic control cif a structure possible. This paper discusses analytical investigations that are focused on the development of improved vibration suppression techniques for flexible spacecraft structures using smart structure actuators and sensors.en_US
dc.rightsThis publication is a work of the U.S. Government as defined
in Title 17, United States Code, Section 101. As such, it is in the
public domain, and under the provisions of Title 17, United States
Code, Section 105, is not copyrighted in the U.S.en_US
dc.titleVibration Suppression: Reduced-Order Model/Residual Mode Filter Control Using Smart Structuresen_US
dc.contributor.departmentDepartment of Mechanical and Aerospace Engineering


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