| タイトル | Active control of buckling of flexible beams |
| 本文（外部サイト） | http://hdl.handle.net/2060/19890006062 |
| 著者（英） | Baz, A.; Tampe, L. |
| 著者所属（英） | Catholic Univ. of America |
| 発行日 | 1989-01-19 |
| 言語 | eng |
| 内容記述 | The feasibility of using the rapidly growing technology of the shape memory alloys actuators in actively controlling the buckling of large flexible structures is investigated. The need for such buckling control systems is becoming inevitable as the design trends of large space structures have resulted in the use of structural members that are long, slender, and very flexible. In addition, as these truss members are subjected mainly to longitudinal loading they become susceptible to structural instabilities due to buckling. Proper control of such instabilities is essential to the effective performance of the structures as stable platforms for communication and observation. Mathematical models are presented that simulate the dynamic characteristics of the shape memory actuator, the compressive structural members, and the associated active control system. A closed-loop computer-controlled system is designed, based on the developed mathematical models, and implemented to control the buckling of simple beams. The performance of the computer-controlled system is evaluated experimentally and compared with the theoretical predictions to validate the developed models. The obtained results emphasize the importance of buckling control and suggest the potential of the shape memory actuators as attractive means for controlling structural deformation in a simple and reliable way. |
| NASA分類 | STRUCTURAL MECHANICS |
| レポートNO | 89N15433
NASA-CR-183333
NAS 1.26:183333 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/143879 |
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