DocumentCode
809592
Title
Applying reliability models to the space shuttle
Author
Schneidewind, Norman F. ; Keller, Ted W.
Author_Institution
US Naval Postgraduate Sch., Monterey, CA, USA
Volume
9
Issue
4
fYear
1992
fDate
7/1/1992 12:00:00 AM
Firstpage
28
Lastpage
33
Abstract
The experience of a team that evaluated many reliability models and tried to validate them for the on-board system software of the National Aeronautics and Space Administration´s (NASA´s) space shuttle is presented. It is shown that three separate but related functions comprise an integrated reliability program: prediction, control, and assessment. The application of the reliability model and the allocation of test resources as part of a testing strategy are discussed.<>
Keywords
aerospace computing; software reliability; NASA; assessment; control; integrated reliability program; on-board system software; prediction; reliability models; space shuttle; test resources; Application software; Certification; Extraterrestrial measurements; History; Performance evaluation; Predictive models; Software performance; Software tools; Space shuttles; Testing;
fLanguage
English
Journal_Title
Software, IEEE
Publisher
ieee
ISSN
0740-7459
Type
jour
DOI
10.1109/52.143099
Filename
143099
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