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Advanced flight control system studyThe architecture, requirements, and system elements of an ultrareliable, advanced flight control system are described. The basic criteria are functional reliability of 10 to the minus 10 power/hour of flight and only 6 month scheduled maintenance. A distributed system architecture is described, including a multiplexed communication system, reliable bus controller, the use of skewed sensor arrays, and actuator interfaces. Test bed and flight evaluation program are proposed.
Document ID
19830007045
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mcgough, J. (Bendix Corp. Teterboro, NJ, United States)
Moses, K. (Bendix Corp. Teterboro, NJ, United States)
Klafin, J. F. (Grumman Aerospace Corp. Bethpage, N.Y., United States)
Date Acquired
September 4, 2013
Publication Date
November 1, 1982
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-CR-163120
NAS 1.26:163120
B-82SRC5
Report Number: NASA-CR-163120
Report Number: NAS 1.26:163120
Report Number: B-82SRC5
Accession Number
83N15316
Funding Number(s)
CONTRACT_GRANT: NAS4-2877
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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