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Journal of Projectiles, Rockets, Missiles and Guidance >

2016 , Vol. 36 >Issue 1: 15 - 18

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2016.01.004

MISSILES AND GUIDANCE TECHNOLOGY

The Simulation Experiment Method of Helicopter-borne Air-to-air Missile Combat Application

  • WANG Lin ,
  • WANG Xiaoqiang ,
  • FU Yafang ,
  • CHEN Lei ,
  • DENG Jianghua
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  • 1 Army Aviation Research Institute, Beijing 101121, China
    2 No.93792 Unit, Hebei Langfang 065000, China

Received date: 2015-03-18

  Online published: 2025-05-30

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Abstract

Simulation experiment method for helicopter-borne air-to-air missile combat application was researched.The main influencing factors of air-to-air missile combat application were systemically analyzed.The semi-practical simulation system of air-to-air missile was established.The experiment design was carried out based on launch condition, target character and battle environment.These experiment context and method could not only meet the requirement of missile combat application, but also provide reference for missile combat application research in the same domain.

Key words： air-to-air missile; combat application; simulation experiment

Cite this article

WANG Lin , WANG Xiaoqiang , FU Yafang , CHEN Lei , DENG Jianghua . The Simulation Experiment Method of Helicopter-borne Air-to-air Missile Combat Application[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2016 , 36(1) : 15 -18 . DOI: 10.15892/j.cnki.djzdxb.2016.01.004

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References

[1]
BALASUBRAMANIAN R, VAIBHAV Shah, KONARK Arora, et al. Numerical investigations of lateral character-istics of an air-to-air missile[J]. Journal of Aircraft, 2013, 50: 88-95.
[2]
BRIAN Michael Birkmire. Air-to-air missile maximum launch range modeling using a multilayer perceptron[C]// AIAA Modeling and Simulation Technologies Confer-ence, 2012: 140.
[3]
王海青, 程梅. 红外导弹仿真试验研究[J]. 飞机设计, 2009, 29(2):57-63.
[4]
马丽华, 乔卫东, 赵尚弘,等. 红外制导半实物仿真及目标模拟器研究[J]. 计算机仿真, 2007, 24(6):42-44.
[5]
方洋旺, 伍友利, 方斌. 机载导弹武器系统作战效能评估[M]. 北京: 国防工业出版社, 2010: 36-37.
[6]
徐宏林. 直升机载武器试验鉴定[M]. 北京: 国防工业出版社, 2012: 288-290.
[7]
JOHN C Gallagher. Air-to-air missile maximum launch range modeling using a multilayer perceptron[C]// AIAA Modeling and Simulation Technologies Conference, 2012: 1-8.
[8]
黄志理, 崔颢, 张平. 武装直升机红外成像仿真[J]. 航空计算技术, 2012, 42(5):106-109.
[9]
樊会涛. 空空导弹方案设计原理[M]. 北京: 航空工业出版社, 2013: 319-322.
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