MISSILES AND GUIDANCE TECHNOLOGY

A Trajectory Tracking Approach Based on Navigation Coordinates for Loitering Munition

  • LI Huaitao ,
  • SUN Jing ,
  • LIU Dawei ,
  • XIA Qunli
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  • 1 School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China
    2 China Research and Development Academy of Machinery Equipment, Beijing 100089, China

Received date: 2015-06-23

  Online published: 2025-05-30

Abstract

To solve the problem of trajectory tracking for loitering munition at constant height, a trajectory tracking approach based on navigation coordinates for loitering munition was put forward.Based on navigation coordinate, omitting azimuth deviation control, two different control strategies were applied to correct lateral deviation in order to ensure the loitering munition flying along ideal trajectory after the whole trajectory was divided into straight line stage and wheeling stage.The simulation result shows that the approach can make sure that during munition flying, the error of deviation from ideal track is quite small and the tacking effect is good.

Cite this article

LI Huaitao , SUN Jing , LIU Dawei , XIA Qunli . A Trajectory Tracking Approach Based on Navigation Coordinates for Loitering Munition[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2016 , 36(3) : 15 -17,21 . DOI: 10.15892/j.cnki.djzdxb.2016.03.005

References

[1]
李佳, 王昊宇, 房玉军. 侦察巡飞弹发展及关键技术分析[J]. 飞航导弹, 2015 (2): 16-20.
[2]
解广华, 邹丹. 巡飞弹发展看点[J]. 轻兵器, 2014 (21): 10-13.
[3]
高晓敏. 新概念信息化弹药的现状与发展[J]. 四川兵工学报, 2008, 29(4): 69-73.
[4]
郭美芳, 彭翠枝. 巡飞弹:一种游弋待机的新型弹药[J]. 现代军事, 2006 (4): 49-52.
[5]
崔生旺, 刘莉. BTT导弹航迹跟踪技术[J]. 弹道学报, 2007, 19(1): 17-20.
[6]
黄叙磊, 王根, 张宝. 巡飞弹航迹导引方法研究[J]. 弹箭与制导学报, 2010, 30(2): 45-48.
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