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Strapdown system Performance Optimization Test evaluations (SPOT), volume 2A three axis inertial system is packaged in an Apollo gimbal fixture for fine grain evaluation of strapdown system performance in dynamic environments. These evaluations have provided information to assess the effectiveness of real-time compensation techniques and to study system performance tradeoffs to factors such as quantization iteration rate. The strapdown performance and tradeoff studies conducted in this program are discussed.
Document ID
19740004242
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Blaha, R. J.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Gilmore, J. P.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1973
Subject Category
Navigation
Report/Patent Number
NASA-CR-136083
R-743-VOL-2
Report Number: NASA-CR-136083
Report Number: R-743-VOL-2
Accession Number
74N12355
Funding Number(s)
PROJECT: DSR PROJ. 55-29435
CONTRACT_GRANT: NAS9-6823
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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