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Integrated assurance assessment of a reconfigurable digital flight control systemThe integrated application of reliability, failure effects and system simulator methods in establishing the airworthiness of a flight critical digital flight control system (DFCS) is demonstrated. The emphasis was on the mutual reinforcement of the methods in demonstrating the system safety.
Document ID
19830016244
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ness, W. G. (Lockheed-Georgia Co. Marietta, GA, United States)
Davis, R. M. (Lockheed-Georgia Co. Marietta, GA, United States)
Benson, J. W. (Lockheed-Georgia Co. Marietta, GA, United States)
Smith, M. K. (Lockheed-Georgia Co. Marietta, GA, United States)
Eldredge, D. (Lockheed-Georgia Co. Marietta, GA, United States)
Date Acquired
September 4, 2013
Publication Date
April 1, 1983
Publication Information
Publisher: FAA
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-CR-170281
AD-A129024
NAS 1.26:170281
Report Number: NASA-CR-170281
Report Number: AD-A129024
Report Number: NAS 1.26:170281
Accession Number
83N24515
Funding Number(s)
CONTRACT_GRANT: NAS2-11179
CONTRACT_GRANT: DOT-FA77WAI-738
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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