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Using Dispersed Modes During Model CorrelationThe model correlation process for the modal characteristics of a launch vehicle is well established. After a test, parameters within the nominal model are adjusted to reflect structural dynamics revealed during testing. However, a full model correlation process for a complex structure can take months of man-hours and many computational resources. If the analyst only has weeks, or even days, of time in which to correlate the nominal model to the experimental results, then the traditional correlation process is not suitable. This paper describes using model dispersions to assist the model correlation process and decrease the overall cost of the process. The process creates thousands of model dispersions from the nominal model prior to the test and then compares each of them to the test data. Using mode shape and frequency error metrics, one dispersion is selected as the best match to the test data. This dispersion is further improved by using a commercial model correlation software. In the three examples shown in this paper, this dispersion based model correlation process performs well when compared to models correlated using traditional techniques and saves time in the post-test analysis.
Document ID
20170001503
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Stewart, Eric C.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Hathcock, Megan L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
February 9, 2017
Publication Date
January 9, 2017
Subject Category
Computer Programming And Software
Launch Vehicles And Launch Operations
Report/Patent Number
M17-5720
Report Number: M17-5720
Meeting Information
Meeting: AIAA SciTech 2017
Location: Grapevine, TX
Country: United States
Start Date: January 9, 2017
End Date: January 13, 2017
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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