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Methods for evaluating integrated airframe/propulsion control system architecturesMethodology, analysis, and detailed design of integrated control system architectures suitable for high-performance aircraft of the 1990s are presented. A methodology, with supporting analytical tools, has been developed to provide system designers with the capability to specify candidate architectures and accurately predict their reliability and performance in the early stages of design development. The authors address the methodology and supporting tools.
Document ID
19880046875
Acquisition Source
Langley Research Center
Document Type
Abstract
Authors
Gerald C Cohen (Boeing (United States) Chicago, Illinois, United States)
Charles W Lee (Boeing (United States) Chicago, Illinois, United States)
Daniel L Palumbo (Langley Research Center Hampton, Virginia, United States)
Date Acquired
August 13, 2013
Publication Date
May 18, 1987
Publication Information
Publication: Proceedings of the IEEE National Aerospace and Electronics Conference
Publisher: Institute of Electrical and Electronics Engineers
URL: https://ieeexplore.ieee.org/servlet/opac?punumber=4871
Subject Category
Aircraft Stability And Control
Meeting Information
Meeting: IEEE National Aerospace and Electronics Conference (NAECON 87)
Location: Dayton, OH
Country: US
Start Date: May 18, 1987
End Date: May 22, 1987
Sponsors: Institute of Electrical and Electronics Engineers
Accession Number
88A34102
Funding Number(s)
CONTRACT_GRANT: NAS1-18099
Distribution Limits
Public
Copyright
Public Use Permitted.

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