GNSS/INS超紧组合导航综述
作者:
作者单位:

(国防科技大学 电子科学学院, 湖南 长沙 410073)

作者简介:

倪少杰(1978—),男,山东莱阳人,研究员,博士,硕士生导师,E-mail:nishaojie123@126.com; 李诗扬(通信作者),男,辽宁丹东人,硕士研究生,E-mail:lishiyang1998@nudt.edu.cn

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中图分类号:

TN967.2

基金项目:

国家自然科学基金资助项目(U20A0193);湖南省自然科学基金资助项目(2021JJ40665)


Overview of GNSS/INS ultra-tight integrated navigation
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(College of Electronic Science and Technology, National University of Defense Technology, Changsha 410073, China)

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    摘要:

    卫星/惯性超紧组合导航系统以其定位精度高、动态性能优良、抗干扰能力强等特性成为组合导航领域的研究热点。介绍了卫星/惯性超紧组合的定位原理,基于对技术原理的分析,比较超紧组合模式相对于其他组合模式的优势特点;以高动态下超紧组合技术及卫星/微惯性单元超紧组合为代表介绍国内外研究现状;总结了亟待研究的容错控制技术、神经网络辅助、多传感器辅助超紧组合等关键技术,并对卫星/惯性超紧组合向着低成本、高精度、强稳定趋势发展的前景进行展望。

    Abstract:

    GNSS/INS ultra-tight integrated navigation system has become a research hotspot in the field of integrated navigation due to its high positioning accuracy, excellent dynamic performance and strong anti-jamming ability. The principle of GNSS/INS ultra-tight integration was introduced, and the advantages and features of ultra-tight integration mode relative to other integration modes were compared based on the analysis of the technical principle. The domestic and international research status was introduced, represented by ultra-tight integration under high dynamics and MIMU/GNSS ultra-tight integration. The key technologies such as fault-tolerant control technology, neural network assistance, and multi-sensor assisted ultra-tight integration were summarized, and the prospect of GNSS/INS ultra-tight integration towards low cost, high precision and strong stability was prospected.

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引用本文

倪少杰,李诗扬,谢郁辰,等. GNSS/INS超紧组合导航综述[J].国防科技大学学报,2023,45(5):48-59.
NI Shaojie, LI Shiyang, XIE Yuchen, et al. Overview of GNSS/INS ultra-tight integrated navigation[J]. Journal of National University of Defense Technology,2023,45(5):48-59.

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  • 收稿日期:2022-09-20
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  • 在线发布日期: 2023-09-26
  • 出版日期: 2023-10-28
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