现代防御技术 ›› 2022, Vol. 50 ›› Issue (6): 50-58.DOI: 10.3969/j.issn.1009-086x.2022.06.007

• 导航、制导与控制 • 上一篇    下一篇

无数据依赖智能技术在机动伴随防空传递对准中的应用

何荧1(), 万佳庆1, 韦姗姗2, 胡晓强3   

  1. 1.江南机电设计研究所, 贵州 贵阳 550009
    2.贵州警察学院, 贵州 贵阳 550009
    3.温州大学 电气与电子工程学院, 浙江 温州 325035
  • 收稿日期:2022-02-20 修回日期:2022-06-10 出版日期:2022-12-28 发布日期:2023-01-06
  • 通讯作者: 何荧
  • 作者简介:何荧(1989-),男,江苏泰州人。高工,博士,研究方向为惯性技术与组合导航。通信地址:550009 贵州省贵阳市经济技术开发区红河路7号 E-mail:yinghe@stu.xmu.edu.cn

Application of Data-Free Intelligent Technology in the Transfer Alignment of Maneuver Concomitant Anti-aircraft

Ying HE1(), Jia-qing WAN1, Shan-shan WEI2, Xiao-qiang HU3   

  1. 1.Jiangnan Electromechanical Design Institute, Guizhou Guiyang 550009, China
    2.Guizhou Police College, Guizhou Guiyang 550009, China
    3.Wenzhou University, College of Electrical and Electronic Engineering, Zhejiang Wenzhou 325035, China
  • Received:2022-02-20 Revised:2022-06-10 Online:2022-12-28 Published:2023-01-06
  • Contact: Ying HE

摘要:

由于机动伴随防空武器系统应用场景的特殊性,难以准确建立适应多变工况的挠曲变形模型,无法保证主子惯导传递对准的精度。为解决这一问题,采用无数据依赖智能技术,将传递对准数学模型中的挠曲变形模型由神经网络代替,神经网络的连接权系数扩充为传递对准模型的部分未知变量,使用非线性卡尔曼滤波对模型所有变量进行实时估计,从而获得主、子惯导之间的失准角,基于主惯导姿态信息进而完成行进中的高精度传递对准。仿真实验表明,该方法能在很短时间内估计出失准角,完成导弹惯导的高精度初始姿态装订。

关键词: 无数据依赖, 传递对准, 神经网络, 挠曲变形, 姿态匹配, 比力匹配

Abstract:

Due to the particularity of the application scenarios of maneuver concomitant anti-aircraft weapon systems, it is difficult to accurately establish a flexural deformation model that adapts to changing working conditions, and the accuracy of transfer alignment cannot be guaranteed. To solve this problem, a data-free intelligent technology is adopted, and the flexural deformation model in the transfer alignment mathematical model is replaced by a neural network. The connection weight coefficients of the neural network are expanded to part of the unknown variables of the transfer alignment model. The nonlinear Kalman filter is used to estimate all the variables of the model in real time, so as to obtain the misalignment angle between the main and the sub-inertial navigation. Based on the attitude information of the main inertial navigation system, the high-precision speed alignment during the movement is completed. Simulation experiments show that this method can estimate the misalignment angle in a short time and complete the high-precision initial attitude binding of the missile inertial navigation system.

Key words: data-free, transfer alignment, neural network, flexural deformation, attitude matching, specific force matching

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