数值微分在设备组合弹道精度评估中的应用
作者:
作者单位:

1.西昌卫星发射中心,四川 西昌 615000;2.重庆大学 自动化学院,重庆 400044

作者简介:

何京江(1970—),女,高级工程师,主要从事航天测控数据处理方向研究,(E-mail)gmy@cqu.edu.cn。

基金项目:

国家自然科学基金重点项目(61633005)。


Numerical differentiation for evaluating theoretical accuracy of device combination trajectory
Author:
Affiliation:

1.Xichang Satellite Launch Center, Xichang, Sichuan 615000, P. R. China;2.College of Automation, Chongqing University, Chongqing 400044, P. R. China

Fund Project:

Supperted by National Natural Science Foundation of China (61633005).

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    摘要:

    设备组合弹道精度评估是测量设备布站设计和设备组合弹道选优方案制定的重要基础。设备组合弹道精度评估通常采用基于误差传播原理的弹道精度评估算法,求解弹道分量关于测元的雅克比矩阵是该算法的核心。然而,对于复杂的弹道方程很难求得雅克比矩阵的解析式。为了解决复杂弹道方程的雅克比矩阵求解难题,提出基于样条数值微分的设备组合弹道精度评估算法,通过构造弹道分量数值队列,进行基于样条插值的数值微分计算出弹道分量关于测元的雅克比矩阵,计算得到设备组合弹道理论精度。最后,通过与单台设备定位方程的理论雅克比矩阵和弹道精度进行对比,验证基于数值微分的设备组合弹道精度评估算法的有效性和实用性。

    Abstract:

    The theoretical accuracy evaluation of device combination trajectories is a critical foundation for device allocation design and trajectory selection. Existing models for accuracy evaluation are based on the error propagation principle, using the Jacobian matrix of the trajectory with respect to measurement elements as their core. However, obtaining the analytic expressions for the Jacobian matrix elements in complex trajectory equations is challenging. This paper proposes and designs a theoretical accuracy evaluation algorithm for device combination trajectories based on numerical differentiation. By constructing numerical sequences and calculating the Jacobian matrix using numerical differentiation with spline interpolation, the theoretical accuracy of the device combination trajectory is determined. The algorithm’s effectiveness and practicality are validated by comparing the Jacobian matrix and accuracy values of the proposed method with those derived from a single device position equation.

    参考文献
    [1] 张金槐. 远程火箭精度分析与评估[M]. 长沙: 国防科技大学出版社, 1995.Zhang J H. Accuracy analysis and evaluation of long range rocket[M]. Changsha: National University of Defense Science and Technology Press, 1995. (in Chinese)
    [2] 刘利生. 外弹道测量数据处理[M]. 北京: 国防工业出版社, 2002.Liu L S. Data processing of exterior ballistic measurement[M]. Beijing: National Defense Industry Press, 2002. (in Chinese)
    [3] 唐雪梅, 蔡洪, 杨华波, 等. 导弹武器精度分析与评估[M]. 北京: 国防工业出版社, 2015.Tang X M, Chai H, Yang H B, et al. Accuracy analysis and evaluation of missile weapon[M]. Beijing: National Defense Industry Press, 2015. (in Chinese)
    [4] 常晓华, 蒋鲁佳, 杨 锐, 等. 垂线偏差对弹道落点精度的影响分析[J]. 国防科技大学学报, 2017, 39(4): 1-5.Chang X H,Jiang L J,Yang R, et al. Analysis on effects of vertical deflection for trajectory impact accuracy[J]. Journal of National University of Defense Technology. 2017, 39(4):1-5. (in Chinese)
    [5] 薛冰, 霍鹏飞, 杨小会. 基于误差合成的射程修正系统精度评估[J]. 探测与控制学报, 2016, 38(4): 58-61.Xue B, Huo P F, Yang X H. Accuracy evaluation of range correction system based on error synthesis[J]. Journal of Detection & Control, 2016, 38(4): 58-61. (in Chinese)
    [6] 雷晓云, 张志安. 基于蒙特卡罗法的一维弹道修正弹落点精度分析[J]. 系统仿真学报, 2016, 28(7): 1685-1691.Lei X Y, Zhang Z A. Research of impact point accuracy of one-dimensional trajectory correction projectile based on Monte Carlo[J]. Journal of System Simulation, 2016, 28(7): 1685-1691. (in Chinese)
    [7] 冯燕来, 王红杰, 李旭等. 基于外弹道修正理论的导弹落点预测精度评估方法[J]. 指挥信息系统与技术, 2017, 8(4): 48-52.Feng Y L, Wang H J, Li X, et al. Precision evaluation method for ballistic missile impact-point prediction based on exterior ballistic correction theory[J]. Command Information System and Technology, 2017, 8(4): 48-52. (in Chinese)
    [8] 郭军海. 弹道测量数据融合技术[M]. 北京: 国防工业出版社, 2012.Guo J H. Ballistic measurement data fusion technology[M]. Beijing: National Defense Industry Press, 2012. (in Chinese)
    [9] 宫志华, 刘洋, 陈春江. 分布式雷达对非合作目标弹道测量精度分析[J]. 弹道学报, 2017, 29(3): 43-48.Gong Z H, Liu Y, Chen C J. Analysis on precision of distributed radar measuring[J]. Ballistic Journal, 2017, 29(3): 43-48. (in Chinese)
    [10] 王子鉴. 多弹头惯性/星光复合制导精度评估与弹道折合方法研究[D]. 长沙: 国防科技大学, 2018.Wang Z J. Study on accuracy evaluation and trajectory conversion of inertial-stellar integrated guidance system based on multiple warheads[D]. Changsha: National University of Defense Science and Technology, 2018. (in Chinese)
    [11] 王若晗. 光电经纬仪系统误差分析及修正方法研究[D]. 西安: 西安理工大学, 2023.Wang R H. Research on system error analysis and correction method of photoelectric theodolite[D]. Xi’an: Xi’an University of Technology, 2023. (in Chinese)
    [12] Ji R P, Liang Y, Xu L F, et al. Trajectory prediction of ballistic missiles using Gaussian process error model[J]. Chinese Journal of Aeronautics, 2022, 35(1): 458-469.
    [13] 张哲, 代洪华, 冯浩阳, 等. 初值约束与两点边值约束轨道动力学方程的快速数值计算方法[J]. 力学学报, 2022, 54(2):503-516.Zhang Z,Dai H H, Feng H Y, et al. Efficient numerical method for orbit dynamic functions with initial value and two-point boundary-value constraints[J]. Journal of Theoretical and Applied Mechanics, 2022, 54(2): 503-516. (in Chinese)
    [14] Saumya R J, Senapati A, Stability, convergence and error analysis of B-spline collocation with Crank-Nicolson method and finite element methods for numerical solution of Schrodinger equation arises in quantum mechanics[J]. Physica Scripta, 2023, 98(11):115232.
    [15] Hosseinian A, Assari P, Dehghan M. The numerical solution of nonlinear delay Volterra integral equations using the thin plate spline collocation method with error analysis[J].Computational and Applied Mathematics,Computational and Applied Mathematics 2023, 42(2): 83.
    [16] 吴开腾. 数值计算方法及其程序实现[M]. 北京: 科学出版社, 2015.Wu K T. Numerical calculation method and its program implementation[M]. Beijing: Science Press, 2015. (in Chinese)
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何京江,杨涵,郭茂耘,柴毅.数值微分在设备组合弹道精度评估中的应用[J].重庆大学学报,2025,48(2):1-9.

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  • 收稿日期:2022-07-23
  • 在线发布日期: 2025-03-04
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