Deployment Simulation Using Absolute Nodal Coordinate Plate Element for Next-Generation Aerospace Structures
Deployment Simulation Using Absolute Nodal Coordinate Plate Element for Next-Generation Aerospace Structures
复制标题
DOI：
10.2514/1.j056477
复制
发表时间：
2017-12
期刊：
影响因子：
2.5
通讯作者：
Keisuke Otsuka;Kanjuro Makihara
中科院分区：
文献类型：
--
作者：
Keisuke Otsuka;Kanjuro Makihara
针对卫星太阳帆板和可展翼飞机等新一代航天结构，提出了一种展开仿真模型。模型采用有限板单元。
In this paper, a deployment simulation model for next-generation aerospace structures, such as satellite solar panels and deployable wing aircraft, is proposed. The model utilizes finite plate elem...