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RAMP: A fault tolerant distributed microcomputer structure for aircraft navigation and controlRAMP consists of distributed sets of parallel computers partioned on the basis of software and packaging constraints. To minimize hardware and software complexity, the processors operate asynchronously. It was shown that through the design of asymptotically stable control laws, data errors due to the asynchronism were minimized. It was further shown that by designing control laws with this property and making minor hardware modifications to the RAMP modules, the system became inherently tolerant to intermittent faults. A laboratory version of RAMP was constructed and is described in the paper along with the experimental results.
Document ID
19800024907
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Dunn, W. R.
(University of Southern Colorado Pueblo, CO, United States)
Date Acquired
September 4, 2013
Publication Date
October 1, 1980
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-CR-163615
Report Number: NASA-CR-163615
Accession Number
80N33415
Funding Number(s)
CONTRACT_GRANT: NAG2-2
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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