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Developing fault models for space mission software

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dc.contributor.author Nikora, A. P. en_US
dc.contributor.author Munson, J. C. en_US
dc.date.accessioned 2004-09-16T23:15:53Z
dc.date.available 2004-09-16T23:15:53Z
dc.date.issued 2003-07-14 en_US
dc.identifier.citation Space Mission Challenges for Information Technology 2003 en_US
dc.identifier.citation Pasadena, CA, USA en_US
dc.identifier.clearanceno 03-1530 en_US
dc.identifier.uri http://hdl.handle.net/2014/7576
dc.description.abstract Over the past several years, we have focused on developing fault models for space mission software. In general, these models use measurable attributes of a software system and its development process to estimate the number of faults inserted into the system during its development; their outputs can be used to better estimate the resources to be allocated to fault identification and removal for all system components. en_US
dc.format.extent 3238139 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other fault models software development software architecture en_US
dc.title Developing fault models for space mission software en_US


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