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Wide angle solar sensorMethod for correcting orientation of spacecraft with respect to sun is discussed. System consists of two photocells on either side of sensor. When photocells are evenly illuminated, no output is made from sensor. When photocells are unevenly illuminated, sensor sends signal to gas jets to change orientation.
Document ID
19720000080
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Schmidt, L. F.
Crawford, W. E.
Date Acquired
August 6, 2013
Publication Date
January 1, 1972
Subject Category
Electronic Components And Circuits
Report/Patent Number
NPO-11341
Report Number: NPO-11341
Accession Number
72B10080
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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