タイトル | Structural dynamics analysis |
本文(外部サイト) | http://hdl.handle.net/2060/19850015527 |
著者(英) | Horner, G.; Belvin, W.; Anderson, M.; Housner, J. M. |
著者所属(英) | NASA Langley Research Center |
発行日 | 1985-04-01 |
言語 | eng |
内容記述 | Dynamic analysis of large space antenna systems must treat the deployment as well as vibration and control of the deployed antenna. Candidate computer programs for deployment dynamics, and issues and needs for future program developments are reviewed. Some results for mast and hoop deployment are also presented. Modeling of complex antenna geometry with conventional finite element methods and with repetitive exact elements is considered. Analytical comparisons with experimental results for a 15 meter hoop/column antenna revealed the importance of accurate structural properties including nonlinear joints. Slackening of cables in this antenna is also a consideration. The technology of designing actively damped structures through analytical optimization is discussed and results are presented. |
NASA分類 | LAUNCH VEHICLES AND SPACE VEHICLES |
レポートNO | 85N23838 |
権利 | No Copyright |