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Standardized strapdown inertial component modularity study, volume 2To obtain cost effective strapdown navigation, guidance and stabilization systems to meet anticipated future needs a standardized modularized strapdown system concept is proposed. Three performance classes, high, medium and low, are suggested to meet the range of applications. Candidate inertial instruments are selected and analyzed for interface compatibility. Electronic packaging and processing, materials and thermal considerations applying to the three classes are discussed and recommendations advanced. Opportunities for automatic fault detection and redundancy are presented. The smallest gyro and accelerometer modules are projected as requiring a volume of 26 cubic inches and 23.6 cubic inches, respectively. Corresponding power dissipation is projected as 5 watts, and 2.6 watts respectively.
Document ID
19740023987
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Feldman, J.
(Draper (Charles Stark) Lab., Inc. Cambridge, MA, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1974
Subject Category
Navigation
Report/Patent Number
R-826-VOL-2
NASA-CR-120428
Report Number: R-826-VOL-2
Report Number: NASA-CR-120428
Accession Number
74N32100
Funding Number(s)
CONTRACT_GRANT: NAS12-2033
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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