欢迎访问《空军工程大学学报》官方网站!

咨询热线:029-84786242 RSS EMAIL-ALERT
基于北斗三号DGNSS/RDSS/INS的高性能轻量级导弹编队基线测量方法
DOI:
作者:
作者单位:

作者简介:

通讯作者:

中图分类号:

TN965

基金项目:

国家自然科学基金(U21A20428)


A Baseline Measurement Method of High Performance Lightweight Missile Formation Based on BDS-3 DGNSS/RDSS/INS
Author:
Affiliation:

Fund Project:

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    在导弹编队基线测量是导弹集群攻击的前提下,针对导弹编队基线测量问题,提出了一种基于北斗三号DGNSS/RDSS/INS的高性能轻量级基线测量方法。以北斗RDSS区域短报文作为编队数传链路,基于北斗三号DGNSS/INS建立伪距单差观测模型,在GNSS信号连续正常或信号中断情况下,进行DGNSS与INS组合导航实现稳定的基线测量输出。仿真结果表明:在GNSS信号连续正常的观测历元中,DGNSS/INS组合导航可以实现稳定的基线测量输出。在GNSS信号中断20 s以内,DGNSS/INS组合导航在东向(E)、北向(N)的基线测量误差小于2.5 m(1σ),天向(U)的基线测量误差小于3.0 m(1σ)。与RTK 算法相比,伪距单差模型对算力的要求降低了70%~80%。

    Abstract:

    Missile formation baseline measurement is the premise of missile cluster attack.In view of the problems in missile formation baseline measurement, a high-performance lightweight baseline measurement method is proposed based on BDS-3 DGNSS/RDSS/INS.Taking the BDS RDSS short message as a formation data transmission link, a pseudo-range single-difference observation model is established based on the BDS-3 DGNSS/INS. Under conditions of continuous normal GNSS signal or signal interruption, the DGNSS and INS integrated navigation is capable of achieving a stable baseline measurement output.The simulation results show that the DGNSS/INS integrated navigation can achieve stable baseline measurement output in the observation epoch of continuous normal GNSS signal. With the GNSS signal interrupting in 20 seconds, the baseline measurement error of DGNSS/INS integrated navigation in the east (E) and north (N) directions is less than 2.5 m(1σ), and the baseline measurement error in the up (U) direction is less than 3.0 m (1σ). The requirement of pseudo-range single-difference model is reduced by 70%~80% compared with the RTK algorithm.

    参考文献
    相似文献
    引证文献
引用本文

张发兴, 李永宁, 肖 勇, 杜 宁, 员 航, 吕 航,秦卫鹏, 李鸿翔, 胡鑫钰, 韩艳蓉.基于北斗三号DGNSS/RDSS/INS的高性能轻量级导弹编队基线测量方法[J].空军工程大学学报,2024,25(2):115-122

复制
分享
文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:
  • 最后修改日期:
  • 录用日期:
  • 在线发布日期: 2024-04-08
  • 出版日期: