DocumentCode
467961
Title
The Dangers of Failure Masking in Fault-Tolerant Software: Aspects of a Recent In-Flight Upset Event
Author
Johnson, C.W. ; Holloway, C. Michael
Author_Institution
Dept. of Comput. Sci., Glasgow Univ., Glasgow
fYear
2007
fDate
22-24 Oct. 2007
Firstpage
60
Lastpage
65
Abstract
On 1 August 2005, a Boeing Company 777-200 aircraft, operating on an international passenger flight from Australia to Malaysia, was involved in a significant upset event while flying on autopilot. The Australian Transport Safety Bureau\´s investigation into the event discovered that "an anomaly existed in the component software hierarchy that allowed inputs from a known faulty accelerometer to be processed by the air data inertial reference unit (ADIRU) and used by the primary flight computer, autopilot and other aircraft systems." This anomaly had existed in original ADIRU software, and had not been detected in the testing and certification process for the unit. This paper describes the software aspects of the incident in detail, and suggests possible implications concerning complex, safety- critical, fault-tolerant software.
Keywords
aerospace computing; aircraft; safety-critical software; software fault tolerance; accelerometer; air data inertial reference unit; aircraft system; autopilot; failure masking; fault-tolerant software; flight computer; safety-critical software;
fLanguage
English
Publisher
iet
Conference_Titel
System Safety, 2007 2nd Institution of Engineering and Technology International Conference on
Conference_Location
London
ISSN
0537-9989
Print_ISBN
978-0-86341-863-1
Type
conf
Filename
4399910
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