NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Dynamic assertion testing of flight control softwareAn experiment in using assertions to dynamically test fault tolerant flight software is described. The experiment showed that 87% of typical errors introduced into the program would be detected by assertions. Detailed analysis of the test data showed that the number of assertions needed to detect those errors could be reduced to a minimal set. The analysis also revealed that the most effective assertions tested program parameters that provided greater indirect (collateral) testing of other parameters.
Document ID
19860013854
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
August 1, 1985
Subject Category
Computer Programming And Software
Report/Patent Number
NASA-CR-176716
SU-CRC-TR-85-15
SU-CSL-TN-85-274
NAS 1.26:176716
Report Number: NASA-CR-176716
Report Number: SU-CRC-TR-85-15
Report Number: SU-CSL-TN-85-274
Report Number: NAS 1.26:176716
Accession Number
86N23325
Funding Number(s)
CONTRACT_GRANT: NAG2-246
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available