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Structural Model Tuning Capability in an Object-Oriented Multidisciplinary Design, Analysis, and Optimization ToolUpdating the finite element model using measured data is a challenging problem in the area of structural dynamics. The model updating process requires not only satisfactory correlations between analytical and experimental results, but also the retention of dynamic properties of structures. Accurate rigid body dynamics are important for flight control system design and aeroelastic trim analysis. Minimizing the difference between analytical and experimental results is a type of optimization problem. In this research, a multidisciplinary design, analysis, and optimization [MDAO] tool is introduced to optimize the objective function and constraints such that the mass properties, the natural frequencies, and the mode shapes are matched to the target data as well as the mass matrix being orthogonalized.
Document ID
20080041519
Acquisition Source
Armstrong Flight Research Center
Document Type
Conference Paper
Authors
Lung, Shun-fat
(NASA Dryden Flight Research Center Edwards, CA, United States)
Pak, Chan-gi
(NASA Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
August 24, 2013
Publication Date
September 14, 2008
Subject Category
Aircraft Design, Testing And Performance
Meeting Information
Meeting: 26th ICAS Congress
Location: Anchorage, AK
Country: United States
Start Date: September 14, 2008
End Date: September 19, 2008
Sponsors: Institute for Computer Applications in Science and Engineering
Distribution Limits
Public
Copyright
Public Use Permitted.
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