反辐射导弹对地攻击中的目标在线估计与协同制导方法

安雅茹 ,  王辉 ,  刘叙含 ,  杨凯

弹道学报 ›› 2025, Vol. 37 ›› Issue (4) : 67 -76.

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弹道学报 ›› 2025, Vol. 37 ›› Issue (4) : 67 -76. DOI: 10.12115/ddxb.2025.10009

反辐射导弹对地攻击中的目标在线估计与协同制导方法

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Online Target Estimation and Cooperative Guidance Method for Anti-radiation Missile in Ground Attack

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摘要

反辐射导弹被动雷达导引头仅能获取目标角度信息,无法测量相对距离,致使目标位置和速度估计精度不足,从而制约打击效能。与此同时,多弹协同打击作为提升敌方雷达摧毁效率的主流作战模式,面临三维协同制导中的通道耦合等挑战。针对上述问题,利用单弹高精度定位与测速信息,采用扩展卡尔曼滤波(extended Kalman filter,EKF)算法实现对目标状态的估计;融合多弹分布式测量数据,采用集中式EKF算法实现多弹协同估计,并对比了纯被动、主动及主被动复合3种导引头配置下的EKF估计精度。同时研究了一种具有攻击角度约束的时间协同制导律,通过设计协同平面和追踪平面,将三维制导律设计转化为二维制导律设计,实现了导弹俯仰通道和偏航通道的解耦;在此基础上构建“在线估计-实时制导”的闭环系统,实现边估计边制导,有效规避误差累积。仿真结果表明,所提出的EKF结合多弹融合方法能够将目标估计位置误差降低50%,收敛速度明显提升,所设计的制导律可实现对雷达目标的有效协同打击,为反辐射导弹的协同制导律设计提供技术支撑。

Abstract

Passive radar seeker used in anti-radiation missile can only acquire target azimuth information without relative range information, making it difficult to precisely determine target position and velocity, thereby limiting strike effectiveness. In addition, although multi-missile coordinated strike represents the mainstream operational approach for enhancing enemy radar destruction efficiency, it faces the challenges such as channel coupling in three-dimensional coordinated guidance. To address these issues, an extended Kalman filter (EKF) algorithm was used to estimate target using high-precision position and velocity data from a single missile. Distributed measurement data from multiple missiles were fused through a centralized EKF framework to achieve cooperative multi-missile state estimation. The estimation accuracy of the EKF was compared across three seeker configurations: purely passive, purely active, and active-passive hybrid. In cooperative guidance design, a time-cooperative guidance law with attack angle constraints was investigated. By designing cooperative and tracking planes, the three-dimensional guidance law was transformed into a two-dimensional problem, thereby decoupling the pitch and yaw channels. A closed-loop “online estimation-real-time guidance” system was established, achieving simultaneous estimation and guidance to eliminate error accumulation. Simulation results demonstrate that the proposed EKF based multi-missile fusion method reduces target position estimation error by 50% and significantly enhances convergence speed. The guidance law enables effective coordinated strikes against radar targets, providing technical support for the design of the guidance law for anti-radiation missile.

关键词

反辐射导弹 / 目标估计 / 协同估计 / 攻击角度约束 / 攻击时间约束

Key words

anti-radiation missile / target estimation / cooperative estimation / attack angle constraint / attack time constraint

引用本文

引用格式 ▾
安雅茹,王辉,刘叙含,杨凯. 反辐射导弹对地攻击中的目标在线估计与协同制导方法[J]. 弹道学报, 2025, 37(4): 67-76 DOI:10.12115/ddxb.2025.10009

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参考文献

[1]

邓瑞静. 反辐射导引头系统仿真及关键技术研究[D]. 西安:西安电子科技大学, 2019.

[2]

DENG Ruijing. Simulation and research on key technology of anti-radiation seeker system[D]. Xi'an: Xidian University, 2019. (in Chinese)

[3]

汪国平, 杨凯, 雷小盈, . 反辐射空地导弹目标无源定位算法及误差分析[J]. 弹箭与制导学报, 2024, 44(3): 66-73.

[4]

WANG Guoping, YANG Kai, LEI Xiaoying, et al. 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. (in Chinese)

[5]

魏政, 杜勇, 刘辉, . 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.

[6]

WEI Zheng, DU Yong, LIU Hui, et al. Development status and analysis of multi-mode composite guidance technology[J]. Aero Weaponry, 2022, 29(6): 26-33. (in Chinese)

[7]

徐骋, 吕腾. 多飞行器打击时刻有限时间一致的协同制导律[J]. 战术导弹技术, 2020(6): 44-52.

[8]

XU Cheng, LV Teng. Cooperative guidance law for multiple UAVs impact times consensus in finite time[J]. Tactical Missile Technology, 2020(6): 44-52. (in Chinese)

[9]

KARBASI M, JAMEI M, MALIK A, et al. Multi-steps drought forecasting in arid and humid climate environments: development of integrative machine learning model[J]. Agricultural Water Management, 2023, 281: 108210.

[10]

秦操. 基于无迹卡尔曼滤波的船舶运动数学模型辨识[J]. 舰船科学技术, 2021, 43(1): 89-94.

[11]

QIN Cao. Parameter identification for ship mathematical model based on unscented Kalman filter[J]. Ship Science and Technology, 2021, 43(1): 89-94. (in Chinese)

[12]

KUPTAMETEE C, AUNSRIN. A review of resampling techniques in particle filtering framework[J]. Measurement, 2022, 193: 110836.

[13]

KALMAN R E, BUCY R S. New results in linear filtering and prediction theory[J]. Journal of Basic Engineering, 1961, 83(1): 95-108.

[14]

NATHAN H, BALAKRISHNAN S N. Impact time and angle guidance with sliding mode control[J]. IEEE Transactions on Control Systems Technology, 2012, 20(6): 1436-1449.

[15]

KUMAR S R, GHOSE D. Sliding mode control based guidance law with impact time constraints[C]// Proceedings of the American Control Conference. Washington, DC: IEEE, 2013.

[16]

KUMAR S R, GHOSE D. Impact time and angle control guidance: AIAA 2015-0616[R]. 2015.

[17]

杨哲. 多约束末制导律与目标状态估计方法研究[D]. 北京:北京理工大学, 2017.

[18]

YANG Zhe. Research on multi-constrained terminal guidance laws and target state estimation methods[D]. Beijing: Beijing Institute of Technology, 2017. (in Chinese)

[19]

BIN Y, WANG H, LIN D, et al. Impact time control guidance against maneuvering targets based on a nonlinear virtual relative model[J]. Chinese Journal of Aeronautics, 2023, 36(7): 444-459.

[20]

DONG W, WANG C, WANG J, et al. Fixed-time terminal angle-constrained cooperative guidance law against maneuvering target[J]. IEEE Transactions on Aerospace and Electronic Systems, 2021, 58(2): 1352-1366.

[21]

LI G, LI Q, WU Y, et al. Leader-following cooperative guidance law with specified impact time[J]. Science China Technological Sciences, 2020, 63(11): 2349-2356.

[22]

YOU H, CHANG X, ZHAO J, et al. Three-dimensional impact-angle-constrained fixed-time cooperative guidance algorithm with adjustable impact time[J]. Aerospace Science and Technology, 2023, 141: 108574.

[23]

YAO H, CHANG X, ZHAO J. Three-dimensional line-of-sight-angle-constrained leader-following cooperative interception guidance law with prespecified impact time[J]. Chinese Journal of Aeronautics, 2025, 38(1): 103151.

[24]

陈之曦, 王健. 纯方位目标跟踪中相对距离的估计方法[J]. 弹道学报, 2025, 37(1): 54-59.

[25]

CHEN Zhixi, WANG Jian. Estimation method for relative distance in bearings-only target tracking[J]. Journal of Ballistics, 2025, 37(1): 54-59. (in Chinese)

[26]

贲思铭, 马国梁, 许立松, . 基于SR-CDKF滤波的弹道目标雷达跟踪算法研究[J]. 弹道学报, 2025, 37(3): 25-32.

[27]

BEN Siming, MA Guoliang, XU Lisong, et al. Research on a ballistic radar target tracking algorithm based on SR-CDKF filter[J]. Journal of Ballistics, 2025, 37(3): 25-32. (in Chinese)

[28]

孙照强, 王志贵, 孟飞, . 基于EF及弹道方程的弹道目标跟踪滤波器设计[J]. 系统工程与电子技术, 2022, 44(10): 3207-3212.

[29]

SUN Zhaoqiang, WANG Zhigui, MENG Fei, et al. Design of track filter for ballistic target based on EKF and ballistic equation[J]. Systems Engineering and Electronics, 2022, 44(10): 3207-3212. (in Chinese)

[30]

董伟. 多约束条件下飞行器协同制导方法研究[D]. 北京:北京理工大学, 2023.

[31]

DONG Wei. Cooperative guidance methods for flight vehicles under multiple constraints[D]. Beijing: Beijing Institute of Technology, 2023. (in Chinese)

基金资助

多模态智能机器人及系统集成教育部集成攻关大平台项目(2024CX02T02)

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