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A note on multicyclic control by swashplate oscillationIt was shown that for two, three, or four bladed rotors, simple oscillation of the nonrotating swashplate controls can produce prescribed blade pitch schedules of the sort which were suggested for vibration alleviation. Equations were given which relate the swashplate motions to the resulting blade pitch schedules.
Document ID
19780013216
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Biggers, J. C. (NASA Ames Research Center Moffett Field, CA, United States)
Mccloud, J. L., III (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1978
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-TM-78475
A-7367
Report Number: NASA-TM-78475
Report Number: A-7367
Accession Number
78N21159
Funding Number(s)
PROJECT: RTOP 505-10-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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