NASA NTRS · 19830000668
Feedback Control of Rotor Overspeed
Abstract
Feedback 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.
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Churchill, G. B.. 1984-11-01. Feedback Control of Rotor Overspeed. https://ntrs.nasa.gov/citations/19830000668
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