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Cost and benefits design optimization model for fault tolerant flight control systemsRequirements and specifications for a method of optimizing the design of fault-tolerant flight control systems are provided. Algorithms that could be used for developing new and modifying existing computer programs are also provided, with recommendations for follow-on work.
Document ID
19820024503
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rose, J. (Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1982
Subject Category
Aircraft Stability And Control
Report/Patent Number
D6-46352
NASA-CR-159281
NAS 1.26:159281
Accession Number
82N32379
Funding Number(s)
CONTRACT_GRANT: NAS1-15506
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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