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Strapdown cost trend study and forecastThe potential cost advantages offered by advanced strapdown inertial technology in future commercial short-haul aircraft are summarized. The initial procurement cost and six year cost-of-ownership, which includes spares and direct maintenance cost were calculated for kinematic and inertial navigation systems such that traditional and strapdown mechanization costs could be compared. Cost results for the inertial navigation systems showed that initial costs and the cost of ownership for traditional triple redundant gimbaled inertial navigators are three times the cost of the equivalent skewed redundant strapdown inertial navigator. The net cost advantage for the strapdown kinematic system is directly attributable to the reduction in sensor count for strapdown. The strapdown kinematic system has the added advantage of providing a fail-operational inertial navigation capability for no additional cost due to the use of inertial grade sensors and attitude reference computers.
Document ID
19750009256
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Eberlein, A. J.
(Honeywell, Inc. Minneapolis, MN, United States)
Savage, P. G.
(Honeywell, Inc. Minneapolis, MN, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1975
Subject Category
Aircraft Communications And Navigation
Report/Patent Number
NASA-CR-137585
Report Number: NASA-CR-137585
Accession Number
75N17328
Funding Number(s)
CONTRACT_GRANT: NAS2-8065
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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