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Dynamic assertion testing of flight control softwareDigital Flight Control System (DFCS) software was used as a test case for assertion testing. The assertions were written and embedded in the code, then errors were inserted (seeded) one at a time and the code executed. Results indicate that assertion testing is an effective and efficient method of detecting errors in flight software. Most errors are eliminate at an earlier stage in the development than before.
Document ID
19860013850
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Andrews, D. M.
(Stanford Univ. CA, United States)
Mahmood, A.
(Stanford Univ. CA, United States)
Mccluskey, E. J.
(Stanford Univ. CA, United States)
Date Acquired
September 5, 2013
Publication Date
July 1, 1985
Subject Category
Computer Programming And Software
Report/Patent Number
NASA-CR-176715
NAS 1.26:176715
SU-HICSS-19
Report Number: NASA-CR-176715
Report Number: NAS 1.26:176715
Report Number: SU-HICSS-19
Accession Number
86N23321
Funding Number(s)
CONTRACT_GRANT: NAG2-246
Distribution Limits
Public
Copyright
Public Use Permitted.
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