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Digital avionics design and reliability analyzerThe description and specifications for a digital avionics design and reliability analyzer are given. Its basic function is to provide for the simulation and emulation of the various fault-tolerant digital avionic computer designs that are developed. It has been established that hardware emulation at the gate-level will be utilized. The primary benefit of emulation to reliability analysis is the fact that it provides the capability to model a system at a very detailed level. Emulation allows the direct insertion of faults into the system, rather than waiting for actual hardware failures to occur. This allows for controlled and accelerated testing of system reaction to hardware failures. There is a trade study which leads to the decision to specify a two-machine system, including an emulation computer connected to a general-purpose computer. There is also an evaluation of potential computers to serve as the emulation computer.
Document ID
19880014088
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 5, 2013
Publication Date
February 1, 1981
Subject Category
Computer Systems
Report/Patent Number
NASA-CR-181641
NAS 1.26:181641
Report Number: NASA-CR-181641
Report Number: NAS 1.26:181641
Accession Number
88N23472
Funding Number(s)
CONTRACT_GRANT: NAS1-15780
PROJECT: RTOP 505-66-21-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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