| 捷联惯性导航计算机小型化设计 |
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| 引用本文： | 李莎,张志鑫,赵博辉.捷联惯性导航计算机小型化设计[J].导航与控制,2014(4):11-16. |
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| 作者姓名： | 李莎 张志鑫 赵博辉 |
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| 作者单位： | 北京航天时代光电科技有限公司;北京航天时代光电科技有限公司;北京航天时代光电科技有限公司 |
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| 摘 要： | 为满足捷联惯性导航计算机的小型化和实时性要求，本文设计了一种使用基于SoC技术设计的A2F500芯片为硬件平台的实现方案。新型的导航计算机与传统的以DSP+FPGA为架构的导航计算机相比，有效地减小了体积，降低了功耗和成本，提高了系统的可靠性，达到了预期的目标,对导航计算机的进一步小型化具有重要意义。
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| 关 键 词： | 导航计算机 SoC 小型化 APB片上总线 |
Design of Micro Strap Inertial Navigation Computer |
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| LI Sh,ZHANG Zhi-xin and ZHAO Bo-hui.Design of Micro Strap Inertial Navigation Computer[J].Navigation and Control,2014(4):11-16. |
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| Authors: | LI Sh ZHANG Zhi-xin and ZHAO Bo-hui |
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| Institution: | Beijing Aerospace Times Optical-electronic Technology CO.,Ltd;Beijing Aerospace Times Optical-electronic Technology CO.,Ltd;Beijing Aerospace Times Optical-electronic Technology CO.,Ltd |
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| Abstract: | For the miniature and real-time requirement of inertia navigation computer, this paper proposed a design of navigation computer on the basis of SoC technology, which is implemented by using A2F500 as the hardware platform. The final design of the navigation computer is characterized by small size, low power consumption ,low system cost and high reliable performance. It can replace the original hardware platform based of DSP&FPGA, and realize navigation functions, and will play great role on the miniature of navigation computer. |
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