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Method for Constructing Composite Response Surfaces by Combining Neural Networks with Polynominal Interpolation or Estimation TechniquesA method and system for data modeling that incorporates the advantages of both traditional response surface methodology (RSM) and neural networks is disclosed. The invention partitions the parameters into a first set of s simple parameters, where observable data are expressible as low order polynomials, and c complex parameters that reflect more complicated variation of the observed data. Variation of the data with the simple parameters is modeled using polynomials; and variation of the data with the complex parameters at each vertex is analyzed using a neural network. Variations with the simple parameters and with the complex parameters are expressed using a first sequence of shape functions and a second sequence of neural network functions. The first and second sequences are multiplicatively combined to form a composite response surface, dependent upon the parameter values, that can be used to identify an accurate mode
Document ID
20070023485
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Rai, Man Mohan
(NASA Ames Research Center Moffett Field, CA, United States)
Madavan, Nateri K.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 23, 2013
Publication Date
March 13, 2007
Subject Category
Aircraft Stability And Control
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-637087
Patent Number: US-Patent-7,191,161
Patent Number: NASA-Case-ARC-14281-3
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-7,191,161|NASA-Case-ARC-14281-3
Patent Application
US-Patent-Appl-SN-637087
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