John E. Bauer

dblp:69/4303 · DBLP profile ↗
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2ranked-venue papers
0as first author
0since 2021 · last 1981
—ORCID · none

Domains — the database's venue-derived domains; a paper can count in several

Systems, architecture and hardware · 2

Expertise — from the expertise taxonomy: the topics of the expert's papers under the CCF categories. A weight counts papers with recency: 1 for a paper about the topic, 0.3 when the topic is its context, halved every five years.

Computer architecture, parallel and distributed computing, and storage systems
1 paper
Electronic design automation · 100%

Topics — the 4 heaviest of 4, each with the papers that count most for it

TopicWeightPapersLastEvidence papers
Electronic design automation › hardware verification and test › design for testability
built-in self-test
0.011975
An Advanced Fault Isolation System for Digital Logic · IEEE Trans. Computers 1975
Electronic design automation › hardware verification and test
fault detection
0.011975
An Advanced Fault Isolation System for Digital Logic · IEEE Trans. Computers 1975
Electronic design automation › hardware verification and test › fault diagnosis
fault isolation
0.011975
An Advanced Fault Isolation System for Digital Logic · IEEE Trans. Computers 1975
Electronic design automation
hardware verification and test
0.011975
An Advanced Fault Isolation System for Digital Logic · IEEE Trans. Computers 1975

Methods — techniques the papers use, named apart from their topics

test pattern generation · 0.0simulation · 0.0
YearPublicationVenuePosition
1981 Parametric Relationships for Self-Contained Test for Digital Avionics Functions
Samuel Kitces, John E. Bauer
ITC2
1975 An Advanced Fault Isolation System for Digital Logic
abstract
Advances in integrated circuit technology are decreasing acquisition cost per function of digital hardware while system software costs are increasing. The hardware advances allow practical implementation of more sophisticated and complex systems which have fewer components, but which may present severe test and maintenance problems due to their complexity. As a result, the use of built-in test (BIT) hardware in place of software becomes increasingly attractive. The Navy funded Advanced Avionics Fault Isolation System (AAFIS) concept utilizes BIT logic for cost-effective fault detection and fault isolation to a digital subsystem and to the faulty module therein. Added logic, available at low cost with advanced microelectronics, is used to perform test pattern generation in each subsystem and to code over the test sequence the outputs and test points on each subsystem module. The coded test response is compared to a predetermined constant. The OR of resulting module pass-fail signals indicates subsystem faults, while identification of a module fail signal provides isolation to a faulty module. Practical coding techniques are presented, with tradeoff of speed, test effectiveness and logic requirements for each. BIT logic design and simulation results verify high fault detection and moderate added logic for BIT.
Norman Benowitz, Donald F. Calhoun, Gary E. Alderson, John E. Bauer, Carl T. Joeckel
IEEE Trans. Computers4