临近空间高超声速滑翔弹跟踪模型

doi:10.3969/j.issn.1009-086x.2018.04.016

现代防御技术 ›› 2018, Vol. 46 ›› Issue (4): 99-106.DOI: 10.3969/j.issn.1009-086x.2018.04.016

临近空间高超声速滑翔弹跟踪模型

喻晨龙^1a, 谭贤四^1b, 王红^1b, 曲智国^1b, 谢非²

1.空军预警学院a.研究生管理大队;b.防空预警装备系,湖北武汉 430019;
2.长江勘测规划设计研究院,湖北武汉 430019

收稿日期:2017-03-27 修回日期:2017-04-26 出版日期:2018-08-30 发布日期:2020-11-25
作者简介:喻晨龙(1989-),男,湖北应城人。博士生,主要从事临近空间高超声速目标预警探测方面研究。通信地址:430019 湖北省武汉市黄浦大街288号空军预警大学研究生大队 E-mail:342583844@qq.com

Tracking Model for Near Space Hypersonic Gliding Missile

YU Chen-long^1a, TAN Xian-si^1b, WANG Hong^1b, QU Zhi-guo^1b, XIE Fei²

1. Air Force Early Warning Academy,a.Department of Graduate Management;b.Department of Air Defense Early Warning Equipment,Hubei Wuhan 430019,China;
2. Changjiang Institute of Survey Planning and Design and Research,Hubei Wuhan 430019,China

Received:2017-03-27 Revised:2017-04-26 Online:2018-08-30 Published:2020-11-25

摘要/Abstract

摘要： 为了提高临近空间高超声速滑翔目标的跟踪精度,基于目标的航迹倾角变化规律建立了一种新的机动模型。为了在雷达测量直角坐标系下估计目标的位置和速度,分析了目标的弹道剖面角,基于航迹倾角变化率和倾角变化率有相近似的变化规律,提出用倾角代替航迹倾角,将倾角变化率描述为零均值正弦自相关随机过程建立角度域的Markov模型,然后将角度关系映射到位置维度建立空间模型。为了使得系统总体状态模型线性,将模型拆分为前端的角度子滤波器和后端的位置子滤波器,由角度滤波器驱动位置滤波器联合跟踪滤波。通过仿真设置了模型的参数,实验结果表明其模型具有更好的跟踪精度。

关键词: 临近空间, 高超声速滑翔目标, 跟踪, 模型, 角度, 位置

Abstract: To improve the tracking accuracy of the hypersonic gliding target in the near space, a novel maneuvering model is established based on the change rule of flight path angle. In order to estimate the position and velocity of the target in the radar measurement coordinate system, the angle of the target's trajectory profile is analyzed. Because of the similar change rule between the change rate of flight path angle and that of the inclination angle, it is proposed to use the inclination angle instead of the flight path angle for establishing the maneuvering model. The change rate of inclination angle is described as a zero mean sinusoidal autocorrelation stochastic process and a Markov model is established. The angular relationship is mapped to the positional dimension for establishing a spatial model. To make the system state model linear, the model is divided into the front-end angle sub-filter and the back-end position sub-filter, and the angle sub-filter drives the position sub-filter for tracking. The parameters of the model are set through simulation. The experimental results show that the model has better tracking accuracy.

Key words: near space, hypersonic gliding target, tracking, model, angle, position

中图分类号:

V412.4
TN953

喻晨龙, 谭贤四, 王红, 曲智国, 谢非. 临近空间高超声速滑翔弹跟踪模型[J]. 现代防御技术, 2018, 46(4): 99-106.

YU Chen-long, TAN Xian-si, WANG Hong, QU Zhi-guo, XIE Fei. Tracking Model for Near Space Hypersonic Gliding Missile[J]. Modern Defense Technology, 2018, 46(4): 99-106.

参考文献

[1] 李建林.临近空间高超声速飞行器发展研究[M].北京:中国宇航出版社,2012.
LI Jian-lin.Research on Development of Near Space Hypersonic Vehicle[M].Beijing:China Aerospace Press,2012.
[2] PAUL L M,VINCENT L R,LUAT T N,et al.NASA Hypersonic Fight Demonstration Overview,Status,and Future Plans[J].Acta Astronautica,2004,55(7):619-630.
[3] 李慧峰.高超声速飞行器制导与控制技术[M].北京:中国宇航出版社,2012.
LI Hui-feng.Hypersonic Vehicles Guidance and Control Technology[M].Beijing:China Aerospace Press,2012.
[4] LI Xiao-rong,JILKOV V P.A Survey of Maneuvering Target Tracking.Part II:Ballistic Target Models[C]//Proceedings of SPIE Conference on Signal and Data Processing of Small Targets,2001,4473:559-581.
[5] OLIVIER D M,ROBERT H B.Tracking and Identification of a Maneuvering Reentry Vehicle[C]//AIAA Guidance,Navigation,and Control Conference and Exhibit,Austin,Texas,USA,2003:1-11.
[6] 张凯,熊家军,韩春耀,等.一种基于气动力模型的高超声速滑翔目标跟踪算法[J].宇航学报,2017,38(2):123-130.
ZHANG Kai,XIONG Jia-jun,HAN Chun-yao,et al.A Tracking Algorithm of Hypersonic Glide Reentry Vehicle via Aerodynamic Model[J].Journal of Astronautics,2017,38(2):123-130.
[7] 李海宁,雷虎民,翟岱亮,等.面向跟踪的吸气式高超声速目标动力学建模[J].航空学报,2014,35(6):1651-1664.
LI Hai-ning,LEI Hu-min,ZHAI Dai-liang,et al.Tracking Oriented Dynamics Modeling of Airbreathing Hypersonic Vehicles[J].Acts Aeronautics et Astronautics Sinica,2014,35(6):1651-1664.
[8] 聂晓华,张夫鸣,徐一鸣.NSHV机动目标跟踪的自适应模型算法[J].系统工程与电子技术,2016,38(3):506-511.
NIE Xiao-hua,ZHANG Fu-ming,XU Yi-ming.Adaptive Model Algorithm for Maneuvering Target Tracking of NSHV[J].Systems Engineering and Electronics,2016,38(3):506-511.
[9] LI Xiao-rong,JILKOV V P.Survey of Maneuver Target Tracking.Part I:Dynamic Models[J].IEEE Transactions on Aerospace and Electronic Systems,2003,39(4):1333-1364.
[10] JILKOV V P,LI Xiao-rong,RU Ji-feng.Modeling Ballistic Target Motion During Boost for Tracking[C]//Proceedings of SPIE Conference on Signal and Data Processing of Small Targets,2007,6699:669909-1-12.
[11] DUAN Zhan-sheng,LI Xiao-rong.Modeling of Farget Motion Constrained on Straight Line[J].IEEE Transactions on Aerospace & Electronic Systems,2016,52(2):548-562.
[12] JILKOV V P,ANGELOVA D S,SEMERDJIEV T A.Design and Comparison of Mode-set Adaptive IMM Algorithms for Maneuvering Target Tracking[J].IEEE Transactions on Aerospace and Electronic Systems,1999,35(1):343-350.
[13] 王国宏,李俊杰,张翔宇,等.临近空间高超声速滑跃式机动目标的跟踪模型[J].航空学报,2015,36(7):2400-2410.
WANG Guo-hong,LI Jun-jie,ZHANG Xiang-yu,et al.A Tracking Model for Near Space Hypersonic Slippage Leap Maneuvering Target[J].Acta Aeronautica et Astronautica Sinica,2015,36(7):2400-2410.
[14] 张翔宇,王国宏,张静,等.临近空间高超声速助推－滑翔式轨迹目标跟踪[J].宇航学报,2015,36(10):1125-1132.
ZHANG Xiang-yu,WANG Guo-hong,ZHANG Jing,et al.Tracking of Hypersonic Boost-to-Glide Trajectory Target in Near-Space[J].Journal of Astronautics,2015,36(10):1125-1132.
[15] 张翔宇,王国宏,李俊杰,等.临近空间高超声速滑跃式机动目标跟踪技术[J].航空学报,2015,36(6):1983-1994.
ZHANG Xiang-yu,WANG Guo-hong,LI Jun-jie,et al.Tracking of Hypersonic Sliding Target in Near-Space[J].Acta Aeronautica et Astronautica Sinica,2015,36(6):1983-1994.
[16] 孙福明,吴秀清,王鹏伟.转弯机动目标的两层交互多模型跟踪算法[J].控制理论与应用,2008,25(2):233-241.
SUN Fu-ming,WU Xiu-qing,WANG Peng-wei.Two-Layer IMM Tracking Algorithm for Turn Maneuver[J].Control Theory & Applications,2008,25(2):233-241.
[17] 齐立峰,惠小平.转弯机动目标跟踪算法研究[J].现代雷达,2014,36(9):40-43.
QI Li-feng,HUI Xiao-ping.A Study on the Algorithm of Corrdinated Turn Motion Tracking[J].Modern Radar,2014,36(9):41-43.[18] JILKOV V P,ANGELOVA D S.Performance Evaluation and Comparison of Variable Structure Multiple-Model Algorithms for Tracking Maneuvering Radar Targets[C] //26th European Microwave Conference.Prague,Czech Republic:IEE Press,1996:332-336.
[19] DUAN Zhan-sheng,LI Xiao-rong.Constrained Target Motion Modeling – Part II:Circular Track[C]//International Conference on Information Fusion,IEEE,2013:2153-2160.
[20] MOHAMMADDADI G,PARIZE N,KARIMPOUR A.Modal Kalman Filter[J].Asian J.Control,2017,19(2):728-738.
[21] JULIER S J,UHLMANN J K.Unscented Filtering and Nonlinear Estimation[J].Proceedings of the IEEE,2004,92(3):401-422.
[22] JIA Bin,XIN Ming,CHENG Yang.High-Degree Cubature Kalman filter[J].Automatica,2013,49(2):510-518.
[23] LI Tian-cheng,SU Jin-ya,LIU Wei,et al.Approximate Gaussian Conjugacy:Parametric Recursive Filtering Under Nonlinearity,Multimode,Uncertainty,and Constraint,and Beyond[J].Frontiers of Information Technology & Electronic Engineering,2017,18(12):1913-1939.

临近空间高超声速滑翔弹跟踪模型

Tracking Model for Near Space Hypersonic Gliding Missile

可视化

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 15

编辑推荐

Metrics

本文评价

[1]	关伟, 林镇明. 加速度计自旋修正系数标定方案分析[J]. 现代防御技术, 2023, 51(4): 104-109.
[2]	刘鹏, 寇鹏飞, 赵凯恒. 舰载相控阵雷达低空测角精度影响因素及改善方法[J]. 现代防御技术, 2023, 51(4): 69-77.
[3]	唐毓燕. 美国陆基中段防御核心能力分析评估[J]. 现代防御技术, 2023, 51(3): 10-19.
[4]	于勇政, 邵学辉, 高仕博, 蒲治伟, 薛冰. 多平台协同跟踪最优构型设计[J]. 现代防御技术, 2023, 51(3): 107-119.
[5]	李碧燕, 胡顺. 基于方向信息的无人机群编队控制算法[J]. 现代防御技术, 2023, 51(2): 55-61.
[6]	梁康博, 杨瑞娟, 李晓柏, 骆伟林, 袁凯. 改进鸽群算法的复杂信号盲源分离[J]. 现代防御技术, 2023, 51(2): 100-108.
[7]	胡文华, 朱常安, 薛东方, 赵喜, 杨瑞. 雷达状态监测与性能综合评估系统的设计与实现[J]. 现代防御技术, 2023, 51(2): 133-140.
[8]	张辉辉, 孙军帅, 王秀鑫, 雷培, 刘鹏飞. 基于模型的系统需求确认与验证技术研究[J]. 现代防御技术, 2023, 51(1): 124-134.
[9]	杨超, 陈小卫, 王超, 徐庆尧, 邢维艳. 航天试验部队训练装备备件军地联合库存建模研究[J]. 现代防御技术, 2023, 51(1): 145-154.
[10]	宋振之, 韩道文, 鲍俊臣, 黄朝阳. 基于改进ADC模型光电对抗系统作战效能评估方法[J]. 现代防御技术, 2023, 51(1): 26-34.
[11]	张耀龙, 阮拥军, 赵陆昊, 黄义松, 郭宇荣. 基于可拓云的合成旅装备保障能力评估方法研究[J]. 现代防御技术, 2023, 51(1): 86-95.
[12]	李宏宇, 尹童, 敦晓彪. 临近空间高超声速武器发展概况与防御体系研究[J]. 现代防御技术, 2022, 50(6): 1-10.
[13]	杨萍, 闫少强, 汪江鹏, 吴丰轩, 阎哲, 燕松. 一种基于安全飞行空间的UAV低空突防改进模型[J]. 现代防御技术, 2022, 50(6): 124-131.
[14]	张书瑞, 杨凡德. 面向远程精确打击的天基信息精准服务研究[J]. 现代防御技术, 2022, 50(6): 59-67.
[15]	季军亮, 李龙跃, 杨小雷, 张微. 改进匈牙利法的多层反导协同作战目标分配模型[J]. 现代防御技术, 2022, 50(5): 59-67.