タイトル | Nonlinearities in spacecraft structural dynamics |
本文(外部サイト) | http://hdl.handle.net/2060/19890004093 |
著者(英) | Taylor, Larry; Latimer, Kelly |
著者所属(英) | George Washington Univ.|NASA Langley Research Center |
発行日 | 1988-10-01 |
言語 | eng |
内容記述 | 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. |
NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
レポートNO | 89N13464 |
権利 | No Copyright |
URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/144498 |