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Precision star-tracking telescopeThe design, construction, and preliminary testing of a new high accuracy star tracking telescope for the laboratory model of the Stanford gyro relativity experiment are described. The function of the telescope in the final flight experiment is to define (by reference to a suitable star) a direction in space for comparison with the relativistic precession of a group of gyroscopes. The design of the telescope has been strongly affected by designs for other portions of the overall experiments, for example the gyroscopes, the attitude control system of the satellite, and the instrumentation system used in processing relativity data. Main goals for the star tracker are: (1) independent readout of angular position in two planes; (2) absolute null stability over a one year period of mechanical parts; (3) readout linear to 0.001 arc-seconds over + or - 0.05 arc-second; (4) noise performance leading to a resolution of 0.05 arc-second in 0.1 second observation time of the chosen reference star; and (5) provision for automatic gain control capable of matching the gains of the gyroscopes and telescope readouts to 1% or better.
Document ID
19720022740
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Fairbank, W. M.
(Stanford Univ. CA, United States)
Everitt, C. W. F.
(Stanford Univ. CA, United States)
Date Acquired
August 6, 2013
Publication Date
July 1, 1972
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-CR-123811
Report Number: NASA-CR-123811
Accession Number
72N30390
Funding Number(s)
CONTRACT_GRANT: NAS8-25705
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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