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Synthesis of individual rotor blade control system for gust alleviationThe utilization of rotor flapping in synthesizing an Individual Blade Control (IBC) system for gust alleviation is demonstrated. The objective is to illustrate and seek to improve Ham's IBC method. A sensor arrangement with two accelerometers mounted on the root and tip of a blade is proposed for estimating of flapping states for feedback control. Equivalent swash plate implementation of IBC is also deliberated. The study concludes by addressing the concept of general rotor states feedback, of which the IBC method is a special case. The blade flapping equation of motion is derived. Ham's original IBC method and a modified IBC scheme called Model Reference (MRIBC) are examined, followed by simulation study with ideal measurements and relative performances of the two methods. The practical aspects of IBC implementation are presented. Different configuration of sensors and their merits are considered. The realization of IBC using equivalent swash plate instead of direct actuator motion is discussed. It is shown that IBC is a particular case of rotor states feedback. The idea of general rotor states feedback is further elaborated. Finally, major conclusions are given.
Document ID
19900016656
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Wang, Ji C.
(San Jose State Univ. CA., United States)
Chu, Alphonse Y.
(San Jose State Univ. CA., United States)
Talbot, Peter D.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1990
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NAS 1.15:101886
NASA-TM-101886
Accession Number
90N25972
Funding Number(s)
CONTRACT_GRANT: NCC2-267
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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