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Microprocessor controlled proof-mass actuatorThe objective of the microprocessor controlled proof-mass actuator is to develop the capability to mount a small programmable device on laboratory models. This capability will allow research in the active control of flexible structures. The approach in developing the actuator will be to mount all components as a single unit. All sensors, electronic and control devices will be mounted with the actuator. The goal for the force output capability of the actuator will be one pound force. The programmable force actuator developed has approximately a one pound force capability over the usable frequency range, which is above 2 Hz.
Document ID
19870013273
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Horner, Garnett C.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1987
Publication Information
Publication: NASA. Marshall Space Flight Center Structural Dynamics and Control Interaction of Flexible Structures
Subject Category
Instrumentation And Photography
Accession Number
87N22706
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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