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Developing Fault Models for Space Mission SoftwareA viewgraph presentation on the development of fault models for space mission software is shown. The topics include: 1) Goal: Improve Understanding of Technology Fault Generation Process; 2) Required Measurement; 3) Measuring Structural Evolution; 4) Module Attributes; 5) Principal Components of Raw Metrics; 6) The Measurement Process; 7) View of Structural Evolution at the System and Module Level; 8) Identifying and Counting Faults; 9) Fault Enumeration; 10) Modeling Fault Content; 11) Modeling Results; 12) Current and Future Work; and 13) Discussion and Conclusions.
Document ID
20070023370
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Nikora, Allen P.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Munson, John C.
(Idaho Univ. Moscow, ID, United States)
Date Acquired
August 23, 2013
Publication Date
July 14, 2003
Subject Category
Computer Programming And Software
Meeting Information
Meeting: Space Mission Challenges for Information Technology
Location: Pasadena, CA
Country: United States
Start Date: July 14, 2003
Distribution Limits
Public
Copyright
Other
Keywords
software measurements
software reliability
software metrics
software fault model

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