BALLISIIC AND AIRDYNAMICS

A Project Trajectory with 2nd-derivative Being Continuous of Large-space Height Descent for Airborne Loitering Munitions

  • CHE Xiaotao ,
  • WANG Xiao ,
  • HAO Feng ,
  • LI Haicheng ,
  • SUN Huyuan
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  • 1 No. 203 Research Institute of China Ordnance Industries, Xi'an 710065, China
    2 Frontier Defence Academy of PLA, Xi'an 710108, China

Received date: 2014-12-16

  Online published: 2025-05-26

Abstract

At the beginning and ending points of large-space height descent trajectory, airborne loitering munitions will oscillate severely and the transition time lasts too long. By researching the height-continuous and the velocity-continuous project trajectory, the physical reasons of those phenomena were analyzed. A novel trajectory for height descent with vertical acceleration being continuous was designed based on trajectory optimization. This height descent project trajectory can realize smooth and quick transition between different trajectories without changing the control system, and it also reduces height overshooting of the loitering munitions. An example was given, validating the effect of this trajectory design method, and it will provide reference for trajectory design of airborne loitering munitions and other similar munitions.

Cite this article

CHE Xiaotao , WANG Xiao , HAO Feng , LI Haicheng , SUN Huyuan . A Project Trajectory with 2nd-derivative Being Continuous of Large-space Height Descent for Airborne Loitering Munitions[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2015 , 35(3) : 138 -142 . DOI: 10.15892/j.cnki.djzdxb.2015.03.035

References

[1]
郭美芳, 彭翠枝. 巡飞弹:一种巡弋待机的新型弹药[J]. 现代军事, 2006(4):49-52.
[2]
慈旋, 周龙, 邵兵. 基于弹道仿真的空舰导弹降高位置研究[J]. 大众科技, 2010(6):68-69.
[3]
王洪强, 邵晓巍, 杨黔龙, 等. 某型滑翔增程靶弹方案弹道设计[J]. 现代防御技术, 2012, 40(2):27-31.
[4]
陈涛, 丁军辉. 当前导弹飞行力学研究中的问题分析[J]. 黑龙江科技信息, 2008(10):44.
[5]
颜仲新, 刘鼎臣. 反舰导弹飞行弹道探讨[J]. 飞航导弹, 2002(2):33-36.
[6]
李一龙, 王光辉, 吕超. 掠海飞行高度对反舰导弹突防能力的影响[J]. 四川兵工学报, 2014, 35(1):45-48.
[7]
钱杏芳. 导弹飞行力学[M]. 北京: 北京理工大学出版社, 2000: 86-87.
[8]
张志涌. 精通 MATLAB R2011a[M]. 北京: 北京航空航天大学出版社, 2013: 130-132.
[9]
谷良贤, 温炳恒. 导弹总体设计原理[M]. 西安: 西北工业大学出版社, 2004: 309-313.
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