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Journal of Projectiles, Rockets, Missiles and Guidance >

2016 , Vol. 36 >Issue 5: 145 - 149,154

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2016.05.037

CORRELATION TECHNOLOGY

Research on Optimizing Operating Range Model of Infrared Detection System

  • WU Xueming ,
  • WANG Haiyan ,
  • KOU Tian ,
  • WANG Fang
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  • Aeronautics and Astronautics Engineering College, Air Force Engineering University, Xi'an 710038, China

Received date: 2015-10-23

  Online published: 2025-05-30

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Abstract

In view of precision and suitability in current operating range model of infrared detection system, realistic band detecting method was applied, and the model based on infrared radiation of target and atmospheric attenuation and detection system performance was built. Characteristic curves of infrared radiation intensity and operating range were acquired by simulation in iterative algorithm The maximum angle of radiation intensity and the farthest detection range were located near tail and deviating from the central axis, and the similar conclusion was acquired by the simulation of aclinic infrared radiation intensity and operating range. Compared with reliable data of similar paper, the optimizing model is realistic and suitable for engineering application

Key words： optics; infrared detection system; infrared radiation intensity; atmospheric attenuation; operating range

Cite this article

WU Xueming , WANG Haiyan , KOU Tian , WANG Fang . Research on Optimizing Operating Range Model of Infrared Detection System[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2016 , 36(5) : 145 -149,154 . DOI: 10.15892/j.cnki.djzdxb.2016.05.037

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References

[1]
SHARP C S, SHAKERNIA O, SASTRY S S. A vision system for landing an unmanned aerial vehicle Proceedings of the 2001 IEEE International Conference on Robotics and Automation, 2001: 1720- 4727.
[2]
SASA S, GOMI H, NINOMIYA T, et al. Position and attitude estimation using image processing of runway: AIAA 2000-0301 R. 2000.
[3]
白亮, 陈袱, 膝科嘉. 计算机视觉辅助无人机自主着陆系统[J]. 弹箭与制导学报, 2006, 26 (2): 320- 321.
[4]
张小苗.机载视觉着陆导航测量方法及关键技术研究［D］.长沙: 国防科学技术大学，2008: 129-150．
[5]
张广军，周富强.基于双圆特征的无人机着陆位置姿态视觉测量方法［J］.航空学报，2005，26( 3) : 344-348．
[6]
蔡鸣，孙秀霞，徐嵩.视觉技术辅助的无人机自主着陆组合导航研究［J］.应用光学，2015，36( 3) : 343-350．
[7]
徐贵力，倪立学，程月华.基于合作目标和视觉的无人飞行器全天候自动着陆导引关键技术［J］.航空学报， 2008，29( 2) : 437-482．
[8]
GUI Y，GUO P Y，ZHANG H L，et al.Airborne visionbased navigation method for UAV accuracy landing using infrared lamps ［J］.Journal of Intelligent ＆Ｒobotic Systems， 2013，72( 2) : 197-218．
[9]
ZHOU X，LEI Z H，YU Q F，et al.Videometric terminal guidance method and system for UAV accurate landing ［C］ ∥ Proc.SPIE 8387， Unmanned Systems Technobgy XIV，2012．
[10]
朱枫，刘昶，吴清潇.视觉约束下无人机位姿参数的后验估计［J］.机器人，2012，34( 4) : 424-431．
[11]
庄丽葵，丁萌，曹云峰.利用地平线与跑道边缘线估计无人机着陆参数［J］.传感器与微系统，2010，29 ( 3) : 104-108．
[12]
李飞，谭乐祖，唐亮.基于跑道灯光的计算机视觉辅助无人机着陆［J］.兵工自动化，2012，31 ( 1 ) :11-13．
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