Structural dynamic responses of a stripped solar sail subjected to solar radiation pressure

被引:11
|
作者
Zhang, Junhui [1 ]
Wu, Na [1 ]
Tong, An [1 ]
Liu, Yinghua [2 ]
机构
[1] North China Univ Technol, Sch Civil Engn, Beijing 100144, Peoples R China
[2] Tsinghua Univ, Sch Aerosp Engn, Beijing 100084, Peoples R China
基金
中国国家自然科学基金;
关键词
Distributed transfer function method; Frequency response; Solar radiation pressure; Solar sail; Structural dynamic response; MODEL;
D O I
10.1016/j.cja.2020.05.003
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The stripped solar sail whose membrane is divided into separate narrow membrane strips is believed to have the best structural efficiency. In this paper, the stripped solar sail structure is regarded as an assembly made by connecting a number of boom-strip components in sequence. Considering the coupling effects between booms and membrane strips, an exact and semi-analytical method to calculate structural dynamic responses of the stripped solar sail subjected to solar radiation pressure is established. The case study of a 100 m stripped solar sail shows that the stripped architecture helps to reduce the static deflections and amplitudes of the steady-state dynamic response. Larger prestress of the membrane strips will decrease stiffness of the sail and increase amplitudes of the steady-state dynamic response. Increasing thickness of the boom will benefit to stability of the sail and reduce the resonant amplitudes. This proposed semi-analytical method provides an efficient analysis tool for structure design and attitude control of the stripped solar sail. (C) 2020 Chinese Society of Aeronautics and Astronautics. Production and hosting by Elsevier Ltd.
引用
收藏
页码:2204 / 2211
页数:8
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