DocumentCode
1870498
Title
Validation of fault tolerance mechanisms of an onboard system
Author
Peng, Junjie ; Ma, Jun ; Hong, Bingrong ; Yuan, Chengjun
Author_Institution
Harbin Inst. of Technol.
fYear
2006
fDate
19-21 Jan. 2006
Lastpage
1234
Abstract
Fault tolerance is of importance to increase the dependability of computer systems. However, it is hard to be evaluated and validated, which will be either time-consuming or costly. Fault injection is an effective method to validate fault tolerance mechanisms. Among different fault injection techniques, software-implemented fault injection (SWIFI) is the most promising one. Although interesting, major drawbacks of existing SWIFI are that temporal and spatial overheads induced into target systems will influence its behavior. In this paper, fault tolerance of an onboard system is tested by a new SWIFI technique which will not induce any additional overheads into the target system under test. The technique is based on embedded processor debug interface standard, Nexus, which ensures that faults are injected into the target system with its behavior being traced while not altering normal execution of the target system
Keywords
aircraft computers; computer debugging; failure analysis; reliability; Nexus; debug standard; embedded processor; fault tolerant mechanism; onboard system; software-implemented fault injection; Computational modeling; Control systems; Electromagnetic radiation; Fault tolerance; Fault tolerant systems; Hardware; Software systems; Software testing; Standards development; System testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Systems and Control in Aerospace and Astronautics, 2006. ISSCAA 2006. 1st International Symposium on
Conference_Location
Harbin
Print_ISBN
0-7803-9395-3
Type
conf
DOI
10.1109/ISSCAA.2006.1627588
Filename
1627588
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