航天器环境工程2023，Vol.40Issue(6)：598-604,7.DOI:10.12126/see.2023069
基于代理模型的批产化卫星动力学试验舱内响应预示方法
A method for internal response prediction based on surrogated model for batch production satellites in dynamics test cabin
摘要
Abstract
In this paper,an internal response prediction method based on surrogate model was proposed for spacecraft structural dynamics test cabin.The feedforward neural network(FNN)and the Kriging model were applied respectively so as to predict the internal measurement point response using actual external measurement data obtained in the sinusoidal sweep frequency test.The prediction results by the two methods were compared through the examples of a component-level product and a system-level spacecraft.The effectiveness of the surrogate prediction method and the influence of sample number on the prediction accuracy were discussed and analyzed.This study may provide a reference for measurement point tailoring in the following dynamics test for batch production spacecrafts.关键词
航天器/动力学环境试验/批严化/测点剪裁/代理模型Key words
spacecraft/dynamics environmental test/batch production/measurement point tailoring/surrogate model分类
航空航天引用本文复制引用
高海洋,孙浩,余小明,许亚娟,郭健龙,马晓荔,何晶,李冬梅..基于代理模型的批产化卫星动力学试验舱内响应预示方法[J].航天器环境工程,2023,40(6):598-604,7.基金项目
2022年度国防科技重点实验室基金项目(编号:2022-JCJQ-LB-075) （编号:2022-JCJQ-LB-075）
