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Feedback Control of Rotor OverspeedFeedback system for automatically governing helicopter rotor speed promises to lessen pilot's workload, enhance maneuverability, and protect airframe. With suitable modifications, concept applied to control speed of electrical generators, automotive engines and other machinery.
Document ID
19830000668
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Churchill, G. B.
Date Acquired
August 11, 2013
Publication Date
November 1, 1984
Publication Information
Publication: NASA Tech Briefs
Volume: 8
Issue: 2
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
ARC-11404
Accession Number
83B10668
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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