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Identification of state variables and dynamic inflow from rotor model dynamic testsThe paper describes methods for extracting unknown state variables and parameters from dynamic rotor model tests given transient cyclic pitch stirring inputs, blade root flap-bending measurements, and the form of the dynamic rotor equations, including a rotor dynamic inflow description, when none of the physical parameters are known. A simplified version of the maximum likelihood method seems best suited for this purpose. The measurement equation error covariance matrix is assumed constant during each iteration, but updated for the subsequent iteration. A detailed analysis of the suitability of the derived techniques for studying various rotor dynamic inflow effects is provided.
Document ID
19770053073
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Banerjee, D.
(Washington Univ. Saint Louis, MO, United States)
Crews, S. T.
(Washington Univ. Saint Louis, MO, United States)
Hohenemser, K. H.
(Washington Univ. Saint Louis, MO, United States)
Yin, S. K.
(Washington University St. Louis, Mo., United States)
Date Acquired
August 9, 2013
Publication Date
April 1, 1977
Publication Information
Publication: American Helicopter Society
Subject Category
Aerodynamics
Accession Number
77A35925
Funding Number(s)
CONTRACT_GRANT: NAS2-7613
Distribution Limits
Public
Copyright
Other

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