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Efficient load measurements using singular value decompositionVarious basic research was performed on efficient load measurement estimation techniques for aircraft structure analysis. An overview is presented of the load measurement problem. Two basic equivalent approaches to load measurement evaluations were considered. Under approach 1, the load values are modeled as depending linearly on the measured values. Under approach 2, the measured values depend linearly on the load values. By using the modern Singular Value Decomposition method, it was shown that under all conditions of the number of loads and number of gages, approach 1 is equivalent to approach 2. By using the conventional normal equation (linear regression) approach, approach 1 is only valid when the number of loads is equal to or greater than the number of gages, while approach 2 is the reverse. Furthermore, except for the case of the number of loads equals the number of gages, the load prediction formulas under the two approaches are not equivalent.
Document ID
19890005424
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Yao, Kung
(California Univ. Los Angeles, CA, United States)
Balakrishnan, A. V.
(California Univ. Los Angeles, CA, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1988
Subject Category
Numerical Analysis
Report/Patent Number
NASA-CR-184614
NAS 1.26:184614
Report Number: NASA-CR-184614
Report Number: NAS 1.26:184614
Accession Number
89N14795
Funding Number(s)
CONTRACT_GRANT: NAG2-433
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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