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双隐身飞机相干干扰对单脉冲雷达影响及影响有效性研究

王春阳 刘明杰 曾会勇 周长霖

王春阳, 刘明杰, 曾会勇, 周长霖. 双隐身飞机相干干扰对单脉冲雷达影响及影响有效性研究[J]. 机械工程学报, 2022, 42(7): 755-763. doi: 10.15918/j.tbit1001-0645.2021.185
引用本文: 王春阳, 刘明杰, 曾会勇, 周长霖. 双隐身飞机相干干扰对单脉冲雷达影响及影响有效性研究[J]. 机械工程学报, 2022, 42(7): 755-763. doi: 10.15918/j.tbit1001-0645.2021.185
WANG Chunyang, LIU Mingjie, ZENG Huiyong, ZHOU Changlin. Influence of Dual Stealth Aircraft Coherent Jamming on Monopulse Radar and Impact Effectiveness Study[J]. JOURNAL OF MECHANICAL ENGINEERING, 2022, 42(7): 755-763. doi: 10.15918/j.tbit1001-0645.2021.185
Citation: WANG Chunyang, LIU Mingjie, ZENG Huiyong, ZHOU Changlin. Influence of Dual Stealth Aircraft Coherent Jamming on Monopulse Radar and Impact Effectiveness Study[J]. JOURNAL OF MECHANICAL ENGINEERING, 2022, 42(7): 755-763. doi: 10.15918/j.tbit1001-0645.2021.185

双隐身飞机相干干扰对单脉冲雷达影响及影响有效性研究

doi: 10.15918/j.tbit1001-0645.2021.185
基金项目: 国家自然科学基金资助项目(61701527)
详细信息
    作者简介:

    王春阳(1967—), 男,博士,教授,博士生导师,E-mail: wangcy_kgd@163.com

    通讯作者:

    刘明杰(1997—) ,男,硕士生,E-mail: 1401628856@qq.com

  • 中图分类号: V218;TN972

Influence of Dual Stealth Aircraft Coherent Jamming on Monopulse Radar and Impact Effectiveness Study

  • 摘要: 针对当前关于双隐身飞机编队相干干扰对单脉冲雷达具体影响分析不足及误差有效性缺乏合理评价的问题,考虑双机回波相位差的随机性特点,建立了双隐身飞机相干干扰模型和角度误差评价模型. 设定双机突防运动场景,提取双机动态RCS,推导回波作用下的双机相干干扰引起的随机性角度误差计算式,求解随机性角度误差的一阶数字特征,并根据脱靶距离建立了角度误差有效性影响评价准则,解算角度误差的有效影响概率. 仿真表明:双隐身飞机相干干扰产生的角度误差均值较大,随机起伏性较弱,干扰效果较好,且误差对雷达影响有效概率较大,保证了编队突防安全性.

     

  • 图  双隐身飞机自卫式干扰场景

    Figure  1.  Dual stealth aircraft self-defense jamming scene

    图  双机纵向编队飞行航迹

    Figure  2.  Dual aircraft longitudinal formation track

    图  双机协同等效干扰场景

    Figure  3.  Dual aircraft coordination equivalent jamming scenario

    图  评价准则示意图

    Figure  4.  Evaluation criteria schematic

    图  隐身飞机时变RCS

    Figure  5.  Stealth aircraft time varying RCS

    图  双隐身飞机回波幅度比

    Figure  6.  Echo amplitude ratio of dual stealth aircraft

    图  信干比

    Figure  7.  Signal to jamming ratio

    图  随机性角度误差均值与标准差

    Figure  8.  Random angle error mean and standard deviation

    图  误差有效影响概率

    Figure  9.  Error effective influence probability

    表  1  飞机巡航参数设置

    Table  1.   Aircraft navigation parameter setting

    机身参数数据
    巡航速度/(m·s−1)500
    隐身飞机编队巡航高度/km10
    隐身飞机编队航路捷径/km32
    纵向编队间距/m280
    巡航时间/s160
    下载: 导出CSV

    表  2  雷达及干扰参数设置

    Table  2.   Radar and interference parameter settings

    参数设置数值
    雷达平均发射功率/kW150
    雷达发射天线增益/dB40
    雷达接收天线增益/dB40
    雷达接收机带宽/MHz5
    隐身飞机St1干扰功率/W50
    隐身飞机St2干扰功率/W50
    单干扰天线增益/dB10
    单干扰设备损耗/dB8
    单干扰频宽/MHz32
    三代机RCS/dBsm16
    下载: 导出CSV
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出版历程
  • 收稿日期:  2021-07-02
  • 刊出日期:  2022-08-17

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