NASA NTRS · 19840048965
Convected transient analysis for large space structures maneuver and deployment
Abstract
Convected-transient analysis techniques in the finite-element method are used to investigate the deployment and maneuver of large spacecraft structures with multiple-member flexible trusses and frames. Numerical results are presented for several sample problems.
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Housner, J.. 1984-01-01. Convected transient analysis for large space structures maneuver and deployment. https://ntrs.nasa.gov/citations/19840048965
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