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Design and implementation of active members for precision space structuresThis paper describes the development and implementation of an active member in a precision truss structure. The active member utilizes a piezoelectric actuator motor imbedded in a steel case with built-in displacement sensor. This active member is used in structural quieting. Collocated active damping control loops are designed in order to impedance match piezoelectric active members to the structure. Results from application of these controllers and actuators to the JPL Phase B testbed are given.
Document ID
19920050687
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Webster, M. S.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Fanson, J. L.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Lurie, B. J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
O'Brien, J. F.
(JPL Pasadena, CA, United States)
Date Acquired
August 15, 2013
Publication Date
February 1, 1992
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 92-1202
Accession Number
92A33311
Distribution Limits
Public
Copyright
Other

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