Passive Target Localization Algorithm and Error Analysis for Anti-radiation Air-to-ground Missile

WANG Guoping; YANG Kai; LEI Xiaoying; SUN Tian

doi:10.15892/j.cnki.djzdxb.2024.03.009

Journal of Projectiles, Rockets, Missiles and Guidance >

2024 , Vol. 44 >Issue 3: 66 - 73

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2024.03.009

Passive Target Localization Algorithm and Error Analysis for Anti-radiation Air-to-ground Missile

WANG Guoping ,
YANG Kai ,
LEI Xiaoying ,
SUN Tian

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Xi’an Mordern Control Technology Research Institute,Xi’an 710065,Shaanxi,China

Received date: 2024-03-13

Online published: 2024-12-28

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Abstract

Aiming at the situation that the anti-radiation missile cannot strike the target effectively in the case of sudden radar shutdown, according to the posture of the helicopter implementing the anti-radiation missile attack, the mathematical model of three-dimensional positioning is constructed, and the passive positioning algorithm is obtained by using the improvement of Kalman filtering derivation, and the simulation verification and analysis are carried out for the positioning accuracy of the altitude angle, azimuth angle, as well as the X, Y, and Z directions before and after the addition of the pure inertial guidance and the combination of the navigation error. After adding pure inertial guidance and combined navigation error, the algorithm is simulated to verify and analyze the positioning accuracy in X, Y, and Z directions before and after filtering. The results show that the accuracy of the proposed passive positioning algorithm based on improved EKF is higher than that of the traditional EKF, the positioning accuracy is less than 4%, and the convergence time is less than 30 s, which meets the demand for passive positioning of antiradiation missile targets, and verifies the feasibility of the algorithm.

Key words： anti-radiation missile; anti-radar shutdown; passive target localization; improved EKF

Cite this article

WANG Guoping , YANG Kai , LEI Xiaoying , SUN Tian . Passive Target Localization Algorithm and Error Analysis for Anti-radiation Air-to-ground Missile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2024 , 44(3) : 66 -73 . DOI: 10.15892/j.cnki.djzdxb.2024.03.009

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References

Publishing order | Descend order by publishing year | Descend order by cited within

[1]	刘万祥, 张永刚,肉孜麦麦提·阿布都嘎依提. 机动雷达抗反辐射导弹研究[J]. 舰船电子对抗, 2022, 45(6): 28-30. LIU W X, ZHANG Y G, ROUZIMEIMETTI·A B D G Y T. Research on mobile radar anti anti-radiation missile[J]. Shipboard Electronic Countermeasure, 2022, 45(6): 28-30.

[2]	魏征, 杜勇, 刘辉, 等. 多模复合制导技术的发展现状与分析[J]. 航空兵器, 2022, 29(6): 26-33. WEI Z, DU Y, LIU H, et al. Development atatus and analysis of multi-mode composite guidance technology[J]. Aero Weaponry, 2022, 29(6): 26-33.

[3]	时磊. 反辐射导弹雷达导引头复杂电磁环境分级方法研究[J]. 船舰电子工程, 2019, 39(8): 180-184. SHI L. Study on the classification method of complex electromagnetic environment of radar seeker in ARM[J]. Ship Electronic Engineering, 2019, 39(8): 180-184.

[4]	侯嵬, 毕大平, 赵禄达. 基于改进Vague集的弹道导弹突防阶段电子防御效能评估[J]. 电讯技术, 2022, 62(7): 915-921. HOU W, BI D P, ZHAO L D. Assessment of ballistic missile electronic defense effectiveness in penetrating period based on improved vague set[J]. Telecommunication Engineering, 2022, 62(7): 915-921.

[5]	王勃, 朱学平, 杨军. 基于自适应UKF的反辐射无人机抗雷达关机技术研究[J]. 计算机测量与控制, 2012, 20(7): 1960-1962. WANG B, ZHU X P, YANG J. Study of anti-radiation UAV based on adaptive UKF to against radar switching off[J]. Computer Measurement and Control, 2012, 20(7): 1960-1962.

[6]	杨林冲, 王清海. 反辐射导弹对抗雷达关机技术研究[J]. 航空兵器, 2016(1): 13-17. YANG L C, WANG Q H. Research on against radar shutdown technique of anti radiation missile[J]. Aviation Weapon, 2016(1): 13-17.

[7]	叶俊. 一种改进的自适应UKF被动定位方法[J]. 电讯技术, 2020, 60(4): 428-432. YE J. An improved passive location method using adaptive unscented Kalman filter[J]. Telecommunication Engineering, 2020, 60(4): 428-432.

[8]	王榕, 杨林冲, 鲁建辉. 毫米波导引头在空地末制导中捕获区与纵向机动能力分析[J]. 电光与控制, 2014, 21(7): 78-80. WANG R, YANG L C, LU J H. Analysis of acquisition area and longitudinal maneuvering capability of millimeter wave seeker in air-to-ground terminal guidance[J]. Electro-optics and Control, 2014, 21(7): 78-80.

[9]	李康, 丁国如, 李京华, 等. 无源定位技术发展动态及其应用分析[J]. 航空兵器, 2021, 28(2): 104-112. LI K, DING G R, LI J H, et al. Development dynamics of passive positioning technology and its application analysis[J]. Aviation Weapon, 2021, 28(2): 104-112.

[10]	钱志鸿, 孙大洋, LEUNG V. 无线网络定位综述[J]. 计算机学报, 2016, 39(6): 1237-1256. QIAN Z H, SUN D Y, LEUNG V. A review of wireless network localization[J]. Journal of Computing, 2016, 39(6): 1237-1256.

[11]	汪子嘉. 基于无线传感网的无源定位关键技术研究[D]. 郑州: 解放军信息工程大学, 2013. WANG Z J. Research on key technology of passive localization based on wireless sensor network[D]. Zhengzhou: PLA Information Engineering University, 2013.

[12]	张艳如. 机载无源定位内场测试方法[J]. 中国科技信息, 2022, 33(19): 57-59. ZHANG Y R. Internal field test method of airborne passive positioning[J]. China Science and Technology Information, 2022, 33(19): 57-59.

[13]	沈文亮, 李艳斌. 基于无源测距的快速定位方法研究[J]. 电子学报, 2009, 6(37): 43-47. SHEN W L, LI Y B. Research on fast localization method based on passive ranging[J]. Electronic Journal, 2009, 6(37): 43-47.

[14]	郭行, 黄静雯, 陈康, 等. 一种反辐射导弹抗低截获概率雷达关机的被动定位方法[J]. 指挥控制与仿真, 2013, 35(6): 100-104 GUO X, HUANG J W, CHEN K, et al. Passive orientation of anti-radiation missile against low probability of intercept radar’s shutdown[J]. Command Control and Simulation, 2013, 35(6): 100-104.

[15]	周颖, 甘德云, 许保民, 等. 反辐射武器攻防对抗理论与试验[M]. 北京: 电子工业出版社, 2012. ZHOU Y, GAN D Y, XU B M, et al. Theory and experiment of offensive and defensive confrontation of anti-radiation weapons[M]. Beijing: Electronic Industry Press, 2012.

[16]	孙琳, 李小波, 周青松, 等. 基于扩展卡尔曼滤波的雷达无源定位方法[J]. 火力与指挥控制, 2016, 41(11): 58-61. SUN L, LI X B, ZHOU Q S, et al. Radar passive location method based on extended Kalman filter[J]. Fire Control and Command Control, 2016, 41(11): 58-61.

[17]	RISTIC B, SANJEEV M. Tracking a manoeuvring target using angle-only measurements: algorithms and performance[J]. Elsevier, Signal Processing, 2003, 83(6): 1223-1238.

[18]	SONG T L, UM T Y. Practical guidance for homing missile with bearing only measurement[J]. IEEE Transaction on Aerospace and Electronic Systems(S0018-9251), 1996, 32(1): 434-444.

[19]	VADDI S S, MENON P K. Target state estimation for integrated guidance-control of missiles: AIAA 2007-6838[R]. Reston: AIAA, 2007.

[20]	秦永元, 张洪钺, 汪叔华. 卡尔曼滤波与组合导航原理[M]. 西安: 西北工业大学出版社, 1998: 34-35. QIN Y Y, ZHANG H Y, WANG S H. Kalman filter and integrated navigation principle[J]. Xi’an: Northwestern Polytechnical University Press, 1998: 34-35.

[21]	毛玉良. 激光陀螺捷联惯导系统误差辨识与修正技术研究[D]. 北京: 北京理工大学, 2014. MAO Y L. Research on error identification and correction technology of laser gyro strapdown intertial navigation system[D]. Beijing: Beijing Institute of Technology, 2014.

[22]	董一平, 刘宁, 苏中, 等. 基于AEKF的高速自旋飞行体组合导航方法[J]. 系统工程与电子技术, 2022, 44(6): 1977-1983. DOI DONG Y P, LIU N, SU Z, et al. Integrated navigation method of high speed spin aircraft based on AEKF[J]. Systems Engineering and Electronics, 2022, 44(6): 1977-1983.

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