南华大学学报（自然科学版）Issue(3)：103-110,8.
空间薄膜结构展开分析模型研究综述
Study on Analysis Model of Deployable Space Membrane Structure
摘要
Abstract
With the rapid development of space membrane structures,how to effectively im-plement the deployment of space membrane structures have become more and more impor-tant and one of the key technical issues of concern to aerospace engineering. If the space membrane structure cannot be reliably deployed,it will directly affect the performance of the spacecraft such as accuracy, signal transmission, etc. , and for the spacecraft to com-plete the space mission as expected has very important significance. In this paper,several international theoretical and experimental analysis models of deployment of common space membrane structures were reviewed,particularly comparative analysis of several major mod-els such as fluent-solid coupling model,spring-mass model,control volume model and ener-gy-momentum model,were conducted from the theoretical base,practical applications,and advantages and disadvantages of other aspects. Some proposed amendments to the corre-sponding recommendations for further space to analyze membrane structure has important theoretical and practical reference guide.关键词
空间薄膜结构/展开分析/模型/研究进展Key words
space membrane structures/deployment/analysis model分类
通用工业技术引用本文复制引用
肖潇,关富玲..空间薄膜结构展开分析模型研究综述[J].南华大学学报（自然科学版）,2015,(3):103-110,8.基金项目
民用航天科研预先研究基金资助项目( C1320060312) （ C1320060312）
国家安监总局安全生产重大事故防治关键技术科技基金资助项目(hunan-0021-2014AQ) （hunan-0021-2014AQ）
湖南省科技计划基金资助项目(2014GK3111) （2014GK3111）
衡阳市科技计划基金资助项目(2014KS24) （2014KS24）
