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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 requirements to be validated down to the design level.
Document ID
20210003577
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
External Source(s)
Authors
Holzlmann, Gerard J.
Callahan, John R.
Easterbrook, Steve M.
Schneider, Francis
Date Acquired
April 6, 1998
Publication Date
April 6, 1998
Publication Information
Publisher: UNKNOWN
Distribution Limits
Public
Copyright
Other
Technical Review
Keywords
Fault
Tolerant
Systems
Model
Checking

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