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Actuators for actively controlled space structuresA free-flying platform of about 4 x 17 m overall dimensions, carrying a variety of imaging and sounding payloads, calls for an intelligent structure with active dynamic control of structural resonances. The actuators for such a structure must be lightweight, require low power, and allow integration into the structure without degradation of its integrity; the dc-to-100 Hz dynamic range required may entail several types of actuators, as is presently emphasized. Broadband damping of higher-order modes requires modeling of the structure with a distributed array of sensors and actuators.
Document ID
19870055542
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Studer, P.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Sharma, R.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Baz, A.
(Catholic University of America, Washington, DC, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
87A42816
Distribution Limits
Public
Copyright
Other

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