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Performance evaluation of a strapdown electrically suspended gyro for spaceThe engineering development directed to improvement in strapdown electrically suspended gyro (SD/ESG) readout accuracy are described. The results of this development effort were represented by new and modified parts which were assembled into a strapdown ESG which was evaluated in terms of its readout system accuracy. The program performance goal was the demonstration of gyro readout to an accuracy of 15 arc-seconds or better. The results of calibrating over two sets of data were error amounts of 11.4 and 12.7 arc-seconds rms. The rms values of readout error were 12.7 and 13.8 arc-seconds for two sets of data not included in the calibration. The techniques for rotor preparation which were investigated under this contract included the application of a thin metal coating to the rotor surface in addition to the use of bare, polished beryllium rotors. Patterning application means which were utilized included a laser for pattern exposure of a photoresist coating and a grit-blast patterning machine which applied the pattern directly onto the metal surface of the rotor.
Document ID
19730011994
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Elwell, D. F.
(Honeywell, Inc. Saint Petersburg, FL, United States)
Wacker, J. C.
(Honeywell, Inc. Saint Petersburg, FL, United States)
Miletich, J. M.
(Honeywell, Inc. Saint Petersburg, FL, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1973
Subject Category
Navigation
Report/Patent Number
NASA-CR-112206
Report Number: NASA-CR-112206
Accession Number
73N20721
Funding Number(s)
CONTRACT_GRANT: NAS1-11078
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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