Publication Date:
2013-08-31
Description:
In considering nonlinearities in spacecraft structural dynamics, the following are examined: (1) SCOLE Configuration-Equations of Motion; (2) Modeling Error Sources; (3) Approximate Solutions; (4) Comparison of Model Accuracy; (5) Linear and Nonlinear Damping; (6) Experimental Results; and, (7) Future Work.
Keywords:
SPACECRAFT DESIGN, TESTING AND PERFORMANCE
Type:
Proceedings of the 4th Annual SCOLE Workshop; p 67-101
Format:
application/pdf
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