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一种基于非线性回归的载人航天器密封舱内在轨噪声分析方法

李喆 柏林厚 李兴乾 张昊 曲溪 于泓淼

航天器环境工程2017,Vol.34Issue(1):63-69,7.
航天器环境工程2017,Vol.34Issue(1):63-69,7.DOI:10.3969/j.issn.1673-1379.2017.01.010

一种基于非线性回归的载人航天器密封舱内在轨噪声分析方法

A analysis method of on-orbit noise in manned spacecraft pressurized cabin based on non-linear regression

李喆 1柏林厚 1李兴乾 1张昊 1曲溪 1于泓淼1

作者信息

  • 1. 中国空间技术研究院载人航天总体部,北京 100094
  • 折叠

摘要

Abstract

The noise inside a manned spacecraft pressurized cabin in orbit is an important issue for astronauts. In this paper, a non-linear regression analysis method for the noise in the manned spacecraft pressurized cabin is proposed. From the noise data of a manned spacecraft pressurized cabin, the on-orbit position-noise math model is built by this method. It is shown that the noise deviation between the value calculated by the on-orbit math model and the value measured by test is less than 4%. The model could offer predicted on-orbit noise data for the noise reduction design, the noise simulation and the noise reduction measure verification on the ground stage.

关键词

载人航天器/密封舱/在轨噪声/非线性回归分析

Key words

manned spacecraft/pressurized cabin/on-orbit noise/nonlinear regression analysis

分类

航空航天

引用本文复制引用

李喆,柏林厚,李兴乾,张昊,曲溪,于泓淼..一种基于非线性回归的载人航天器密封舱内在轨噪声分析方法[J].航天器环境工程,2017,34(1):63-69,7.

基金项目

国家重大科技专项工程 ()

航天器环境工程

OACSTPCD

1673-1379

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