Abstract
A finite element methodology developed to model the dynamic behavior of flexible articulated structures is briefly presented. It is then used to simulate the deployment of large space structures. Its efficiency is demonstrated on three application cases representative of space engineering.
| Original language | English |
|---|---|
| Pages (from-to) | 61-66 |
| Number of pages | 6 |
| Journal | American Society of Mechanical Engineers, Pressure Vessels and Piping Division (Publication) PVP |
| Volume | 176 |
| State | Published - 1989 |
| Externally published | Yes |
| Event | Seismic Engineering - 1989: Design, Analysis, Testing, and Qualification Methods - Honolulu, HI, USA Duration: 23 Jul 1989 → 27 Jul 1989 |