Hardware Fault Insertion and Instrumentation System: Mechanization and Validation

Benson, J. W.

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Hardware Fault Insertion and Instrumentation System: Mechanization and Validation

1987-03-01
By Benson, J. W.

File Language:

English

Details

Creators:

Benson, J. W.
Corporate Creators:

Lockheed-California Company
Corporate Contributors:

United States. Department of Transportation. Federal Aviation Administration. Technical Center
Subject/TRT Terms:

Aeronautics Airborne Navigational Aids Data Fault Tolerance Software Testing Validation
Publication/ Report Number:

DOT/FAA/CT-86/31
Resource Type:

Tech Report
Geographical Coverage:

United States
Corporate Publisher:

United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center
Abstract:

This effort was performed to provide automated test capability for extensive low-level hardware fault insertion testing. The capability developed was applied in a related task that is described in DOT/FAA/CT-86/34. The test capability was used to calibrate fault detection coverage and associated latency times as relevant to projecting overall system reliability.
Format:

PDF
Collection(s):

FAA William J. Hughes Technical Center for Advanced Aerospace
Main Document Checksum:

urn:sha-512:27d862bd79597ff2cf31314ba4450c5f741582cefc29d459dbb8901295889de4ee66a95692e09497902123b399978051999929ab0f3d0af354ae25c280c59c97
Download URL:

https://rosap.ntl.bts.gov/view/dot/92740/dot_92740_DS1.pdf
File Type:

[PDF - 843.08 KB ]

File Language:

English

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