Jiang Xiangjun, Pan Fengqun, Fan Yesen, Du Jingli, Zhu Mingbo, Chen Zhen
Key Laboratory of Electronic Equipment Structural Design, Xidian University, Xi'an 710071, China.
Xi'an Institute of Space Radio Technology, Xi'an 710100, China.
Materials (Basel). 2019 Aug 16;12(16):2619. doi: 10.3390/ma12162619.
The high surface accuracy design of a cable-net antenna structure under the disturbance of the extremely harsh space environment requires the antenna to have good in-orbit adjustment ability for surface accuracy. A shape memory cable-net (SMC) structure is proposed in this paper and believed to be able to improve the in-orbit surface accuracy of the cable-net antenna. Firstly, the incremental stiffness equation of a one-dimensional bar element of the shape memory alloy (SMA) to express the relationship between the force, temperature and deformation was effectively constructed. Secondly, the finite element model of the SMC antenna structure incorporated the incremental stiffness equation of a SMA was established. Thirdly, a shape active adjustment procedure of surface accuracy based on the optimization method was presented. Finally, a numerical example of the shape memory cable net structure applied to the parabolic reflectors of space antennas was analyzed.
在极端恶劣的空间环境干扰下,索网天线结构的高表面精度设计要求天线具有良好的在轨表面精度调整能力。本文提出了一种形状记忆索网(SMC)结构,认为其能够提高索网天线的在轨表面精度。首先,有效构建了形状记忆合金(SMA)一维杆单元的增量刚度方程,以表达力、温度和变形之间的关系。其次,建立了包含SMA增量刚度方程的SMC天线结构有限元模型。第三,提出了基于优化方法的表面精度形状主动调整程序。最后,分析了形状记忆索网结构应用于空间天线抛物面反射器的数值算例。