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弹道学报  2014 

基于在线修正弹道模板的主动段弹道跟踪方法

Keywords: 弹道导弹,主动段,弹道模板,在线修正

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Abstract:

为了提高在线跟踪主动段弹道导弹的精度,提出了基于在线修正的弹道模板方法,详细构建了空气动力、推力、重力、科氏力、牵连惯性力等的动力学模型,结合不敏卡尔曼滤波和粒子滤波算法,对弹道模板参数进行在线校正及对导弹目标进行实时跟踪。在仿真过程中,基于加加速度模型和当前统计模型构建了交互多模型算法,并将该算法结合不敏卡尔曼滤波和粒子滤波算法与在线修正的弹道模板方法进行比较分析。仿真结果表明,该方法能够对弹道模板参数进行准确估计并能获得比交互多模型算法更高的跟踪精度。

References

[1]  张涛,安玮,周一宇.主动段弹道定位与跟踪算法[J].弹道学报,2005,17(4):11-16.
[2]  ZHANG Tao,AN Wei,ZHOU Yi-yu.The trajectory locating and tracking algorithm in boost phase[J].Journal of Ballistics,2005,17(4):11-16.(in Chinese)
[3]  陈映,程臻,文树梁.弹道导弹助推段同时跟踪和类型识别算法研究[J].信号处理,2011,27(5):749-754.
[4]  CHEN Ying,CHENG Zhen,WEN Shu-liang,Study on method for simultaneously tracking and classifying ballistic missile in boost and post-boost phase[J].Signal Processing,2011,27(5):749-754.(in Chinese)
[5]  陈映,文树梁,程臻.一种适用于助推段弹道导弹的跟踪方法研究[J].系统仿真学报,2012,24(5):1 063-1 067.
[6]  CHEN Ying,WEN Shu-liang,CHENG Zhen.Method for tracking ballistic missile on boost phase[J].Journal of System Simulation,2012,24(5):1 063-1 067.(in Chinese).
[7]  LI X R,JILKOV V P.A survey of maneuvering target tracking,part Ⅱ:ballistic target models[J].SPIE,2001,4 473:559-581.
[8]  LI X R,JILKOV V P.A survey of maneuvering target tracking,part Ⅲ:measurements models[J].SPIE,2001,4 473:423-446.
[9]  JOHN A,LUKACS I V.Hit-to-kill guidance for the interception of ballistic in the boost phase[D].Monterey,CA:Naval Postgraduate Shool,2006.
[10]  张毅,杨辉耀,李俊莉.弹道导弹弹道学[M].长沙:国防科大出版社,1999:111-157.
[11]  ZHANG Yi,YANG Hui-yao,LI Jun-li.The ballistic trajectory[M].Changsha:National University of Defense Technology Press,1999:111-157.(in Chinese).
[12]  郭尊华,谢维信.弹道导弹跟踪技术进展[J].信号处理,2009,25(8a):578-581.
[13]  GUO Zun-hua,XIE Wei-xin.Ballistic missile tracking:a review[J].Signal Processing,2009,25(8a):578-581.(in Chinese)
[14]  周宏仁,敬忠良,王培德.机动目标跟踪[M].北京:国防工业出版社,1991.
[15]  ZHOU Hong-ren,JING Zhong-liang,WANG Pei-de.Mobile target tracking[M].Beijing:National Defense Industry Press,1991.(in Chinese)
[16]  申镇,强胜,易东云.基于运动方程的单星无源主动段射向估计方法[J].弹道学报,2010,22(1):7-10.
[17]  SHEN Zhen,QIANG Sheng,YI Dong-yun.Course head estimation method based on movement equation by single satellites passive detection in boost phase[J].Journal of Ballistics,2010,22(1):7-10.(in Chinese)
[18]  张涛,安玮,周一宇,等.基于推力加速度模板的主动段弹道跟踪方法[J].宇航学报,2006,27(3):385-389.
[19]  ZHANG Tao,AN Wei,ZHOU Yi-yu,et al.Periodic relative motion condition for satellites formations considering nonlinearity[J].Journal of Astronautics,2006,27(3):385-389.(in Chinese)
[20]  张涛,安玮,周一宇.基于UKF的主动段弹道跟踪算法[J].弹道学报,2006,18(2):15-18.
[21]  ZHANG Tao,AN Wei,ZHOU Yi-yu.Trajectory tracking method in boost phase by using UKF[J].Journal of Ballistics,2006,18(2):15-18.(in Chinese)

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