DocumentCode
2815283
Title
Real-time software failure characterization
Author
Dunham, Janet R. ; Finelli, George B.
fYear
1990
fDate
25-28 June 1990
Firstpage
39
Lastpage
45
Abstract
An overview of a series of studies aimed at characterizing the fundamentals of the software failure process is presented. The focus is on the development of three independent implementations of an aerospace guidance and control software (GCS) application. The study addresses three objectives related to the development of a credible software reliability assessment methodology: description, development method effectiveness, and fundamentals. Previous studies have provided insight about the software failure process. Different faults were found to produce errors at widely varying rates. Program error rates were found to follow a log-linear trend with respect to the number of faults corrected. Some of the faults were found to interact with each other in concealing and revealing ways. Points in the input space that cause a fault to produce errors can tend to cluster and form regions called error crystals.<>
Keywords
aerospace computer control; program testing; real-time systems; software reliability; GCS; aerospace computer control; credible software reliability assessment methodology; development method effectiveness; error crystals; error rates; guidance/control software; independent implementations; input space; log-linear trend; real-time software failure characterization; software failure process; Aerospace control; Computer errors; Fault tolerance; Fault tolerant systems; NASA; Navigation; Petroleum; Pressing; Software reliability; Vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Computer Assurance, 1990. COMPASS '90, Systems Integrity, Software Safety and Process Security., Proceedings of the Fifth Annual Conference on
Conference_Location
Gaithersburg, MD, USA
Type
conf
DOI
10.1109/CMPASS.1990.175400
Filename
175400
Link To Document