航天器环境工程Issue(1)：67-71,5.DOI:10.3969/j.issn.1673-1379.2015.01.013
星载感应式磁力仪电控学箱设计与分析
Design and analysis of electronic control cabinet for spaceborne induction magnetometer
摘要
Abstract
In order to provide a good environment for the electronic components of the induction magnetometer on orbit, and to protect the equipment against the impact load during the satellite launch process, it is desirable to design an electronic control cabinet with superior thermal, mechanical and anti-radiation performances. A related design for the electronic control cabinet is presented in this paper, which combine the circuit design, the structural design and the thermal design, with optimized system performance. By thermal and mechanical simulations, the design is validated, and it is shown that the structural and thermal designs of the electronic control cabinet can fully meet the relevant index requirements. This design method of the electronic control cabinet for the spaceborne induction magnetometer can also be used for the design of other electronic devices.关键词
感应式磁力仪/电控学箱/结构设计/热设计Key words
induction magnetometer/electronic control cabinet/structural design/thermal design分类
航空航天引用本文复制引用
何江飞,曾立,魏丽,符璇..星载感应式磁力仪电控学箱设计与分析[J].航天器环境工程,2015,(1):67-71,5.基金项目
国家自然科学基金资助项目 （）
