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彈載衛星導航設備電磁干擾治理技術(shù)
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上海機電工程研究所

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    摘要:

    隨著(zhù)彈載電子設備集成化發(fā)展趨勢,彈上計算機、衛星導航等設備在狹小空間內功能緊密耦合,多源多頻段信號傳輸發(fā)生干擾造成導航設備無(wú)法準確定位的現象時(shí)常發(fā)生,針對這一問(wèn)題,本文系統研究了衛星導航設備電磁干擾治理方法。首先研究了微機模塊中開(kāi)關(guān)電源與隔離器件的電磁輻射以及諧波干擾特性;其次,基于電磁波金屬介質(zhì)傳播原理,通過(guò)COMSOL軟件建立了設備電磁屏蔽有限元模型,深度剖析了屏蔽體電導率、厚度、開(kāi)孔等關(guān)鍵因素對屏蔽效能的影響規律,進(jìn)而提出關(guān)鍵元器件設計、終端天線(xiàn)屏蔽等綜合治理方法;最后以彈載衛星導航產(chǎn)品進(jìn)行試驗,干擾信號強度得到了抑制,設備定位測速成功率提高了85%,驗證了治理方法的科學(xué)合理性。

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    With the development of integration of the electronic equipment on missile, due to the functions of microcomputer and satellite navigation module couples close in a small space, multi-source multi-frequency band signals interference with each other, which sometimes caused that the navigation equipment cannot be accurately positioned. To solve the problem, this paper studys systematically the electromagnetic interference (EMI) control methods for the integrated electronic equipments on missiles. Firstly, the electromagnetic radiation and harmonic interference characteristics of switching power supply and isolation devices in the circuit. Secondly, based on the electromagnetic wave propagation principle in metal media, electromagnetic shielding finite element model is established by COMSOL software, the influence of shield’s conductivity, thickness, openings and other key factors on the shielding effectiveness are analyzed. Then comprehensive approaches to EMI management such as key component design and terminal antenna shielding are proposed. Finally, a set of integrated electronic equipment is test and the results show that the interference signal intensity is reduced, the equipment positioning speed success rate is increased by 85%, verifying the scientific rationality of the proposed methods.

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石現,梁旗,蔡克榮,楊昌達,葛宇航,張澤凱,于峰,季飚.彈載衛星導航設備電磁干擾治理技術(shù)計算機測量與控制[J].,2024,32(12):216-222.

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歷史
  • 收稿日期:2024-07-29
  • 最后修改日期:2024-08-23
  • 錄用日期:2024-08-27
  • 在線(xiàn)發(fā)布日期: 2024-12-24
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