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The inclusion of semi-Markov reconfiguration transitions into the computer-aided Markov evaluator (CAME) programThe modifications to the rule-based CAME program which allow it to more accurately model the fault-handling processes of fault-tolerant systems are described. This new capability is added to the CAME program by modeling the fault-handling processes of fault-tolerant systems. The integrated airframe/propulsion control system architecture (IAPSA II) reference configuration currently under development is detailed.
Document ID
19890030742
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rosch, Gene (Draper (Charles Stark) Lab., Inc. Cambridge, MA, United States)
Hutchins, Monica A. (Draper (Charles Stark) Lab., Inc. Cambridge, MA, United States)
Leong, Frank J. (Draper (Charles Stark) Lab., Inc. Cambridge, MA, United States)
Babcock, Philip S., IV (Charles Stark Draper Laboratory, Inc. Cambridge, MA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1988
Subject Category
Computer Programming And Software
Report/Patent Number
AIAA PAPER 88-3906
Meeting Information
Meeting: AIAA/IEEE Digital Avionics Systems Conference
Location: San Jose, CA
Country: United States
Start Date: October 17, 1988
End Date: October 20, 1988
Accession Number
89A18113
Funding Number(s)
CONTRACT_GRANT: NAS9-17560
Distribution Limits
Public
Copyright
Other

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