Transient dynamic analysis of gossamer appendage deployment using nonlinear finite element method

被引：0

作者：

Sakamoto, Hiraku ^{[1
]}

Miyazaki, Yasuyuki ^{[2
]}

Mori, Osamu ^{[3
]}

机构：

[1] Department of Mechanical and Aerospace Engineering, Structural Dynamics Design Laboratory, Tokyo Institute of Technology, 2-12-1 #I3-17 Ookayama, Meguro-ku, Tokyo 152-8552, Japan

[2] Department of Aerospace Engineering, College of Science and Technology, Nihon University, 7-24-1 Narashinodai, Funabashi, Chiba 274-8501, Japan

[3] Lunar and Planetary Exploration Group, Japan Aerospace Exploration Agency, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

来源：

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference | 2009年

关键词：

D O I：

2009-2170

中图分类号：

学科分类号：

摘要：

Transient analysis - Stiffness - Structural dynamics - Finite element method

引用