NASA NTRS · 19870013294
Structural dynamics system model reduction
Abstract
Loads analysis for structural dynamic systems is usually performed by finite element models. Because of the complexity of the structural system, the model contains large number of degree-of-freedom. The large model is necessary since details of the stress, loads and responses due to mission environments are computed. However, a simplified model is needed for other tasks such as pre-test analysis for modal testing, and control-structural interaction studies. A systematic method of model reduction for modal test analysis is presented. Perhaps it will be of some help in developing a simplified model for the control studies.
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Chen, J. C., Rose, T. L., Wada, B. K.. 1987-04-01. Structural dynamics system model reduction. https://ntrs.nasa.gov/citations/19870013294
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