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Surface accuracy measurement system deployable reflector antennasConceptual optical sensor configurations for measuring the surface deformations of large, deployable space antennas are described. These antennas include precision deployable reflectors up to 30 meters diameter and 1000 GHz frequency and mesh deployable reflectors up to 100 meters diameter and 30 GHz frequency. For each representative antenna configuration, the surface deformation sensor provides continuous, real-time measurements at a sufficient number of sample points to be compatible with active surface control. Moreover, the sensor system does not interfere with the mechanical or microwave characteristics of either the antenna surface or the feed. For the applications considered, the sensor system consists of a central receiver ring containing six to ten long focal length, angle measuring instruments, each viewing a dedicated set of bright point targets at the antenna. The targets, either light emitting diodes or illuminated retroreflectors, are modulated to eliminate errors from spurious backgrounds. Very preliminary performance estimates indicate that the sensor system, using commerical grade components, can produce a 20th to a 30th wavelength accuracy (3 sigma).
Document ID
19790050742
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Neiswander, R. S.
(TRW Defense and Space Systems Group Redondo Beach, Calif., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Subject Category
Spacecraft Instrumentation
Report/Patent Number
AIAA PAPER 79-0937
Meeting Information
Meeting: Conference on Advanced Technology for Future Space Systems
Location: Hampton, VA
Start Date: May 8, 1979
End Date: May 10, 1979
Accession Number
79A34755
Funding Number(s)
CONTRACT_GRANT: NAS1-15520
Distribution Limits
Public
Copyright
Other

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