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Inductive Linear-Position Sensor/Limit-Sensor UnitsA new sensor provides an absolute position measurement. A schematic view of a motorized linear-translation stage that contains, at each end, an electronic unit that functions as both (1) a non-contact sensor that measures the absolute position of the stage and (2) a non-contact equivalent of a limit switch that is tripped when the stage reaches the nominal limit position. The need for such an absolute linear position-sensor/limit-sensor unit arises in the case of a linear-translation stage that is part of a larger system in which the actual stopping position of the stage (relative to the nominal limit position) must be known. Because inertia inevitably causes the stage to run somewhat past the nominal limit position, tripping of a standard limit switch or other limit sensor does not provide the required indication of the actual stopping position. This innovative sensor unit operates on an electromagnetic-induction principle similar to that of linear variable differential transformers (LVDTs)
Document ID
20100011127
Acquisition Source
Marshall Space Flight Center
Document Type
Other - NASA Tech Brief
Authors
Alhom, Dean
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Howard, David
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Smith, Dennis
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Dutton, Kenneth
(Sverdrup Technology, Inc. United States)
Date Acquired
August 24, 2013
Publication Date
October 1, 2007
Publication Information
Publication: NASA Tech Briefs, October 2007
Subject Category
Instrumentation And Photography
Report/Patent Number
MFS-32102-1
Distribution Limits
Public
Copyright
Public Use Permitted.
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