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.
Originalsprache | Englisch |
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Seiten (von - bis) | 61-66 |
Seitenumfang | 6 |
Fachzeitschrift | American Society of Mechanical Engineers, Pressure Vessels and Piping Division (Publication) PVP |
Jahrgang | 176 |
Publikationsstatus | Veröffentlicht - 1989 |
Extern publiziert | Ja |
Veranstaltung | Seismic Engineering - 1989: Design, Analysis, Testing, and Qualification Methods - Honolulu, HI, USA Dauer: 23 Juli 1989 → 27 Juli 1989 |