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Structural Alignment Sensor Feasibility DemonstrationA structural alignment sensor (SAS) was developed for use with large deployable antenna systems for contour measurement and/or active control. The SAS is a laser ranging system using frequency modulation and accurate phase measurement to determine distance. Work was done with a CO2 and HeNe laser. The capability of the SAS to measure antenna rib contours was studied over ranges of 50 meters to a resolution of 100 microns. Initial resolution data was taken with the CO2 system. This data shows that it will indeed meet the SAS requirements. The development of the HeNe system was initiated because it offers substantial improvement in size, weight, and power over the CO2 system. The final demonstration was made with the HeNe system and it too showed that the SAS requirements could be met with this alternate approach. The projection of these results to a conceptual design for a flight system and its application are described.
Document ID
19790011286
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Anderson, R. H.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Huang, C. C.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Hodor, J. R.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1978
Subject Category
Energy Production And Conversion
Report/Patent Number
NASA-CR-158353
LMSC-D644951
Report Number: NASA-CR-158353
Report Number: LMSC-D644951
Accession Number
79N19457
Funding Number(s)
CONTRACT_GRANT: NAS7-100
CONTRACT_GRANT: JPL-955130
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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