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Improvement of helicopter attitude stability by active control of the conventional swash plateThe Final Report on improvement of helicopter attitude stability by active control of the conventional swash plate covering the period from Nov. 1986 to Dec. 1993 is presented. A paper on the history, principles, and applications of helicopter individual-blade-control is included.
Document ID
19940016051
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ham, Norman D. (Massachusetts Inst. of Tech. Cambridge, MA, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1993
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-CR-194786
NAS 1.26:194786
VTL-TR-198-6
Report Number: NASA-CR-194786
Report Number: NAS 1.26:194786
Report Number: VTL-TR-198-6
Accession Number
94N20524
Funding Number(s)
CONTRACT_GRANT: NCC2-447
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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