基于分割法的抛物面固面天线热变形抑制OA北大核心CSTPCD
Thermal deformation suppression of parabolic solid antenna based on the segmentation method
为满足未来高分辨率微波遥感航天器对于大口径高形面精度的空间可展开天线的需求,提出了一种能有效降低偏馈固面天线在轨因热变形造成形面误差的新方法,即分割法.采用5m 口径的偏馈固面抛物面天线,分析了天线热变形对其电性能尤其是主波束效率的影响.对连续固面天线六点支撑下不同支撑位置对其热变形的影响进行了研究.在温差为200 ℃的均匀温度场下,分析了不同形状单胞的形面误差,随后确认采用正六边形作为分割单胞并对其形面误差与尺寸的关系进行了研究.研究了分割单胞的尺寸及排布方式对天线的形面误差及电性能的影响,并验证了分割单胞之间的缝隙对天线电性能的影响,最终确定分割方案.结果显示,分割后天线形面误差从500μm降低至5μm,主波束效率下降值从6.72%下降至1.77%.
To meet the demands of large-aperture,high surface accuracy of deployable antennas for high-resolution microwave remote sensing spacecraft in the future,a novel method called segmented method was proposed,which can effectively reduce the surface error caused by thermal deformation of the solid partial feed antenna in orbit.A parabolic solid partial feed antenna with a 5m aperture was employed,and then the effect of thermal deformation on the electrical performance of the antenna,especially the main beam efficiency,was analyzed with the finite element method.The influence of the support method with six points on the thermal deformation of the continuous solid surface antenna was investigated.Under the uniform temperature field with a difference of 200℃,the surface errors of cells with different shapes were analyzed,and then a hexagon shape was adopted as a segmented cell and the relationship between the surface error and the size was studied.The surface error and electrical performance of the antenna after being segmented by single cells with different sizes and arrangements were investigated,the effect of the splits among the segmented cells on the electrical performance of the antenna was verified,and the final segmented configuration was determined.The results show that the surface error decreases from 500 pm to 5 pm and the main beam efficiency decreases from 6.72%to 1.77%through the final segmented configuration.
楼春钢;李昊;潘殿坤
宁波大学冲击与安全工程教育部重点实验室,宁波 315211上海卫星工程研究所,上海 201109
空间可展开天线高形面精度热变形分割法主波束效率
space deployable antennahigh surface accuracythermal deformationsegmented methodmain beam efficiency
《中国空间科学技术》 2024 (002)
59-67 / 9
中国博士后科学基金(2020M681805)
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