NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
A Process for Verifying and Validating Requirements for Fault Tolerant Systems Using Model CheckingModel checking is shown to be an effective tool in validating the behavior of a fault tolerant embedded spacecraft controller. The case study presented here shows that by judiciously abstracting away extraneous complexity, the state space of the model could be exhaustively searched allowing critical functional requirement to be validated down to the design level.
Document ID
20060040554
Acquisition Source
Jet Propulsion Laboratory
Document Type
Reprint (Version printed in journal)
External Source(s)
Authors
Schneider, F.
Easterbrook, S.
Callahan, J.
Holzmann, G.
Reinholtz, W.
Ko, A.
Shahabuddin, M.
Date Acquired
August 23, 2013
Publication Date
February 1, 1999
Publication Information
Publication: Transactions on Software Engineering
Subject Category
Computer Programming And Software
Distribution Limits
Public
Copyright
Other
Keywords
model checking fault tolerant embedded spacecraft controller validation

Available Downloads

There are no available downloads for this record.
No Preview Available