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Qualification of the flight-critical AFTI/F-16 digital flight control systemQualification considerations for assuring the safety of a life-critical digital flight control system include four major areas: systems interactions, verification, validation, and configuration control. The AFTI/F-16 design, development, and qualification illustrate these considerations. In this paper, qualification concepts, procedures, and methodologies are discussed and illustrated through specific examples.
Document ID
19830035274
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mackall, D. A. (NASA Flight Research Center Edwards, CA, United States)
Ishmael, S. D. (NASA Flight Research Center Edwards, CA, United States)
Regenie, V. A. (Systems Control Technology, Inc. Edwards, CA, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1983
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA PAPER 83-0060
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting
Location: Reno, NV
Start Date: January 10, 1983
End Date: January 13, 1983
Accession Number
83A16492
Distribution Limits
Public
Copyright
Other

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