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导引模型在FTC自适应IMM-UKF目标跟踪算法中的应用
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  • 英文篇名:Application of Guidance Model in FTC Adaptive IMM- UKF Maneuvering Target Tracking Algorithm
  • 作者:付斌 ; 丁月宁 ; 黄勇 ; 闫杰
  • 英文作者:FU Bin;DING Yue-ning;HUANG Yong;YAN Jie;Northwestern Polytechnical University;
  • 关键词:目标跟踪 ; 导引运动模型 ; 交互多模型滤波 ; 弹道收敛因子
  • 英文关键词:target tracking;;guidance model;;interacting multiple model;;factor of trajectory convergence
  • 中文刊名:DGKQ
  • 英文刊名:Electronics Optics & Control
  • 机构:西北工业大学航天学院;
  • 出版日期:2014-01-06 15:37
  • 出版单位:电光与控制
  • 年:2014
  • 期:v.21;No.187
  • 基金:航空科学基金(20110153004)
  • 语种:中文;
  • 页:DGKQ201401018
  • 页数:6
  • CN:01
  • ISSN:41-1227/TN
  • 分类号:72-76+81
摘要
在应用IMM算法时,根据战术导弹这种特殊的应用对象,以两种常用导引律为例,推导出导引运动模型作为交互模型集;使用不敏卡尔曼滤波器(UKF)实现了IMM-UKF算法,并根据导引模型的特点引入了弹道收敛因子(FTC)自适应调节IMM算法中的模型转移概率。仿真实验结果表明,这种基于目标导引运动模型的跟踪算法很好地实现了目标跟踪任务,并且有效地分辨出了目标机动的运动模型。
        This paper presents a new approach of the Interacting Multiple Model( IMM) algorithm by introducing a non-linear guidance model from the guidance law. Unscented Kalman Filter( UKF) is applied to deal with the non-linear models in the IMM algorithm. Factor of Trajectory Convergence( FTC) is introduced based on the basic characteristic of the missile trajectory to adjust the transition probability online. The simulation results demonstrate that the guidance model based FTC adaptive IMM-UKF algorithm works perfectly in the tracking system.
引文
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