航空航天
航空航天工程
可控性
软件部署
空格(标点符号)
太阳帆
系统工程
计算力学
机械工程
工程类
计算机科学
航天器
结构工程
数学
有限元法
应用数学
操作系统
软件工程
作者
Bing Wang,Juncheng Zhu,Shuncong Zhong,Wei Liang,Chenglong Guan
标识
DOI:10.1016/j.matdes.2023.112557
摘要
Space deployable structures are able to be deployed from a folded state to a predetermined or desired configuration. They are superior in terms of spatial packaging ratio, controllability, and structural complexity, in order to solve the space limitations for aerospace vehicles. Therefore, they have been applied in structural designs and concepts for various aerospace missions, including space support booms, space deployable antennas, solar panels, as well as flexible solar sails. Recent development of advanced manufacturing technologies and applications of novel smart materials and structures, brings new degree of design freedom to space deployable mechanics, inspiring novel space deployable mechanisms, especially for smart driving and control strategies. Here, we present a review on development of mechanics and smart driving of space deployable structures. Advantages and limitations for various deployable mechanisms are also presented to reveal further insights. The trends and future deployable mechanics are directed by further advancements in terms of modularisation, intelligences, and deployment precision. Multi-disciplinary cross-integrations are leading the way for future breakthroughs in novel deployable mechanics and intelligent driving control for space explorations.
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