Developing fault models for space mission software

Nikora, A. P.; Munson,  J. C.

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