Publikationsdatum:
2019-07-13
Beschreibung:
The objective of the present methodology is two-fold: (1) to process test data obtained from either modal survey tests, or slow sine-sweep tests, to extract a set of orthogonal modes best matching the test data while being commensurate with the dynamic model, and (2) to modify submatrices of the dynamic model mass and stiffness matrices to adjust the model to best fit the test data. The method has been implemented using a linear statistical sequential estimator for computation on a CDC computer. Demonstration problems involving Space Shuttle quarter-scale vibration test data and dynamic models have been run. This paper will discuss the general methodology and experience to date.
Schlagwort(e):
GROUND SUPPORT SYSTEMS AND FACILITIES (SPACE)
Materialart:
SAE PAPER 781047
,
Society of Automotive Engineers, Aerospace Meeting; Nov 27, 1978 - Nov 30, 1978; San Diego, CA
Format:
text
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