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基于自适应滤波的高超声速滑翔目标三维跟踪算法
引用本文:张君彪,熊家军,兰旭辉,李凡,刘文俭,席秋实.基于自适应滤波的高超声速滑翔目标三维跟踪算法[J].系统工程与电子技术,2022,44(2):628-636.
作者姓名:张君彪  熊家军  兰旭辉  李凡  刘文俭  席秋实
作者单位:1. 空军预警学院研究生大队, 湖北 武汉 4300192. 空军预警学院四系, 湖北 武汉 4300193. 中国人民解放军95980部队, 湖北 襄阳 441000
基金项目:军队重点科研课题(KJ20191A020148);军事类研究生(JY2019B138)资助课题。
摘    要:针对临近空间高超声速滑翔飞行器机动模式复杂,单一运动学模型难以完成三维跟踪的问题,提出一种三维跟踪方法.将飞行器机动弹道分为纵向和横向弹道,根据飞行器机动特性,在纵向上将加速度建模为零均值的二阶时间自相关随机过程,在横向上采用Singer模型和匀加速模型进行交互多模型(interactive multiple mode...

关 键 词:临近空间  高超声速飞行器  三维跟踪  滤波算法  交互多模型
收稿时间:2020-06-15

3D tracking algorithm of hypersonic gliding target based on adaptive filtering
ZHANG Junbiao,XIONG Jiajun,LAN Xuhui,LI Fan,LIU Wenjian,XI Qiushi.3D tracking algorithm of hypersonic gliding target based on adaptive filtering[J].System Engineering and Electronics,2022,44(2):628-636.
Authors:ZHANG Junbiao  XIONG Jiajun  LAN Xuhui  LI Fan  LIU Wenjian  XI Qiushi
Institution:1. Department of Graduate, Air Force Early Warning Academy, Wuhan 430019, China2. The Fourth Department, Air Force Early Warning Academy, Wuhan 430019, China3. Unit 95980 of the PLA, Xiangyang 441000, China
Abstract:In order to solve the problem that the maneuvering mode of hypersonic gliding vehicle is complex and the single kinematic model is difficult to complete the three-dimensional tracking,a three-dimensional tracking method is proposed.The maneuvering trajectory of the vehicle is divided into longitudinal and lateral trajectory.According to the maneuvering characteristics of the vehicle,the acceleration is modeled as a second-order time autocorrelation stochastic process with zero mean in the longitudinal direction,and the Singer+constant acceleration interactive multiple model(IMM)is used in the lateral direction.The unbiased measurement transformation is introduced to transform the radar observation model in spherical coordinate system to Cartesian coordinate system,which avoids the nonlinear filtering of the model.Finally,based on the existing Kalman filtering,an adaptive Kalman filtering algorithm based on multiple fading factors is designed to enhance the adaptive tracking ability of the model for strong maneuvers.The simulation results show that the algorithm can keep better stability and tracking accuracy when tracking hypersonic gliding target.
Keywords:near space  hypersonic vehicle  three dinensional(3D)tracking  filtering algorithm  interactive multiple model(IMM)
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