Abstract

Due to the wind resistance which acts on the main reflector of large rotary mesh antenna, the correct balancing result of satellite antenna is difficult to be gotten in the ground dynamic balancing test. In order to solve this problem, the dynamic balance method of large rotary mesh antenna which is under the influence of wind resistance in both low pressure environment and standard atmospheric pressure environment on the ground is studied. Based on the theoretical analysis and the experimental data of two-dimensional flow around circular cylinder, a new method of the large rotary mesh antenna wind resistance calculation is proposed, according to the CFD analysis of the three dimensional flow field. Through the dynamic equivalent method, the distributed wind resistance acted on the main reflector of the mesh antenna in the rotating state is equivalent to the principal vector and principal moment of the action point in each quadrant, and then transformed into the eccentric mass on the distribution plane. It provides a feasible and innovative way to estimate the influence of wind resistance on the dynamic balance accuracy of large mesh antenna, so as to compensate the wind resistance effect. Combined with the ground dynamic balancing requirements of a certain type of satellite mesh antenna, the whole finite element model of the mesh antenna is established, the simulation of ground dynamic balancing test is carried out, and the influence of wind resistance on the ground dynamic balancing results of the antenna is analyzed in this study, which provides important data for compensating the influence of wind resistance and ensuring the on-orbit balancing accuracy of the antenna.

Highlights

  • to the wind resistance which acts on the main reflector of large rotary mesh antenna

  • difficult to be gotten in the ground dynamic balancing test

  • the dynamic balance method of large rotary mesh antenna which is under the influence of wind resistance

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Summary

Introduction

3) 叠加得到 A、B 处的合力 FA,FB,即风阻产生 的作用于转轴的等效离心力,如图 9c) 所示。 的有限元模型,依次经过质量属性校核、惯性力载荷 检查、自由模态检查以及工作模态分析等模型验证 环节,天线有限元模型及配平面选取如图 10 所示。 根据静、动不平衡量公式(9) 至(10) ,使用 MATLAB 计算有限元模型中导出的各单元质量、质心信息,并 计算其初始不平衡量。 由于天线结构受限,只能在 有限平面上的特定位置进行质量配平。 通过对比研 究选出最优配平方案:分别取高频箱下表面、副反射 器上 部筋条位置作为配平面, 即坐标分别为 2) 以圆柱绕流试验的阻力系数为计算基础,通 过对各部件 2D、3D 模型的 CFD 分析与试验结果相 对应的方式,完成了各子结构自身及结构与结构间 流场耦合情况下风阻计算的方法修正。 [1] RODRIGUEZ E, STILES B W, DURDEN S L, et al XOVWM: the ⁃generation ocean surface vector winds mission[ C] ∥ 28th Conf on Hurricanes and Tropical Meteorology, Orlando, FL, 2008

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