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A 3D heterogeneously integrated guidance, navigation, and control micro-system

机译:3D异构地集成了指导,导航和控制微系统

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摘要

A GNC micro-system which is developed by 3D heterogeneous integration is presented in this paper. The SRAM, SoC, and FPGA chips are integrated onto a silicon interposer. Other chips are mounted on different MCM substrates. The whole 3D GNC micro-system is packaged using POP technology. The volume is reduced from 120 x 120 x 80 mm(3) to 40 x 40 x 23 mm(3), and the weight is reduced from 1.5 kg to 300 g. The stability of the three axis gyroscopes in the GNC micro-system is 3.11 degrees h(-1), 3.25 degrees h(-1) and 4.26 degrees h(-1), and the accuracy is 5 degrees h(-1). The positioning output stability of the satellite navigation receiver is better than 1 m under static conditions. (C) 2019 The Japan Society of Applied Physics
机译:本文提出了由3D异构集成开发的GNC微系统。 SRAM,SOC和FPGA芯片集成在硅中介层上。其他芯片安装在不同的MCM基板上。整个3D GNC微系统采用POP技术打包。该体积从120×120×80mm(3)减小至40×40×23mm(3),重量从1.5kg减少到300g。 GNC微型系统中的三个轴陀螺仪的稳定性为3.11度H(-1),3.25度H(-1)和4.26度H(-1),精度<5℃(-1) 。卫星导航接收器的定位输出稳定性在静态条件下优于1米。 (c)2019年日本应用物理学会

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  • 来源
    《Japanese journal of applied physics》 |2019年第sh期|SHCB01.1-SHCB01.3|共3页
  • 作者单位

    Xidian Univ Sch Microelect Xian 710071 Shaanxi Peoples R China;

    Beijing Inst Aerosp Control Devices R&D Ctr Beijing 100094 Peoples R China;

    Xidian Univ Sch Microelect Xian 710071 Shaanxi Peoples R China;

    Xidian Univ Sch Microelect Xian 710071 Shaanxi Peoples R China;

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