| 刘革麟,赵荣,田野,谢明,张东.固体姿轨控发动机复杂电磁环境电磁效应分析方法构建研究[J].装备环境工程,2024,21(8):117-126. LIU Gelin,ZHAO Rong,TIAN Ye,XIE Ming,ZHANG Dong.Analysis Method for Complex Electromagnetic Environment of Attitude-orbit Control Engine[J].Equipment Environmental Engineering,2024,21(8):117-126. |
| 固体姿轨控发动机复杂电磁环境电磁效应分析方法构建研究 |
| Analysis Method for Complex Electromagnetic Environment of Attitude-orbit Control Engine |
| 投稿时间：2024-04-23 修订日期：2024-05-14 |
| DOI：10.7643/issn.1672-9242.2024.08.014 |
| 中文关键词: 固体姿轨控发动机 复杂电磁环境 电磁效应 电磁敏感特性 分层解析 耦合干扰矩阵中图分类号:TN011 文献标志码:A 文章编号:1672-9242(2024)08-0117-10 |
| 英文关键词:solid attitude-orbit control engine complex electromagnetic environment electromagnetic effects electromagnetic sensitivity properties layered analysis coupled interference matrix |
| 基金项目: |
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| Author | Institution |
| LIU Gelin | The 210th Institute of the Sixth Academy of CASIC, Xi′an 710065, China |
| ZHAO Rong | The 210th Institute of the Sixth Academy of CASIC, Xi′an 710065, China |
| TIAN Ye | The 210th Institute of the Sixth Academy of CASIC, Xi′an 710065, China |
| XIE Ming | Office of the Eighth Military Representative of the Air Force in the Xi′an Area, Xi′an 710065, China |
| ZHANG Dong | The 210th Institute of the Sixth Academy of CASIC, Xi′an 710065, China |
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| 中文摘要: |
| 目的 构建固体姿轨控发动机不同场景下的复杂电磁环境电磁效应分析方法。方法 通过将固体姿轨控发动机的复杂模型逐层分解，根据各部件级模型的电磁敏感特性，建立电磁敏感度模型。从系统级、整机级、部件级、PCB板级到器件级分析固体姿轨控发动机所面临的复杂环境，并对固体姿轨控发动机电磁特性进行分层解析研究。结果 对固体姿轨控发动机所面临的电磁环境场景进行分类，分为待发射、中段飞行、末段对敌3个主要场景，并对3类场景下的干扰源进行分类，得出复杂电磁环境下固体姿轨控发动机电磁干扰源及敏感体，以及电磁耦合干扰矩阵。结论 本研究对于开展固体姿轨控发动机在复杂电磁环境下的稳定性和可靠性研究具有指导作用，为进一步的电磁特性仿真与验证研究奠定了坚实的基础。 |
| 英文摘要: |
| The work aims to develop analysis methods for analyzing complex electromagnetic environment electromagnetic effects in different scenes of the attitude-orbit control engine construction. By decomposing the complex model of the attitude-orbit control engine layer by layer, electromagnetic sensitivity models were established based on the electromagnetic sensitive characteristics of each component-level model. Analysis was conducted from the system level, the complete machine level, the component level, the PCB board level to the device level to analyze the complex environment faced by the attitude-orbit control engine, and conduct layered analysis research on the electromagnetic characteristics of the attitude-orbit control engine. The electromagnetic environment scenarios faced by the attitude-orbit control engine were classified and divided into three main scenarios:ready-to-launch, mid-flight, and terminal engagement with the enemy. The interference sources under these three types of scenarios were classified, and the electromagnetic interference sources and sensitive bodies as well as the electromagnetic coupling interference matrix of the attitude-orbit control engine under the complex electromagnetic environments were identified. This study provides guidance for the stability and reliability research of the attitude-orbit control engine in complex electromagnetic environments, laying a solid foundation for further electromagnetic characteristics simulation and validation research. |
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