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Design for ValidationThe use of computer hardware and software in life-critical applications, such as for civil air transports, demands the use of rigorous formal mathematical validation procedures. However, formal specification and verification will only be tractable if the system is designed in a manner that lends itself to formal methods. Likewise, accurate reliability analysis will only be tractable if the number of interacting components that must be individually included in a single reliability model is kept to a low number and if their failure behavior interactions can be modeled simply. Also, the system must be designed such that the system reliability does not directly depend on system parameters that cannot be accurately determined. This paper presents a design methodology based on the concept of designing a system in such a manner that it can be rigorously validated, or "design for validation."
Document ID
20040120982
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Johnson, Sally C.
(NASA Langley Research Center Hampton, VA, United States)
Butler, Ricky W.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1991
Subject Category
Computer Programming And Software
Meeting Information
Meeting: 10th Digital Avionics Systems Conference (DASC)
Location: Los Angeles, CA
Country: United States
Start Date: October 7, 1991
End Date: October 11, 1991
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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