首页 | 官方网站   微博 | 高级检索  
     

弹道目标实时跟踪中的滤波方法综述
引用本文:刘也,余安喜,朱炬波,唐歌实.弹道目标实时跟踪中的滤波方法综述[J].宇航学报,2013,34(11):1417-1426.
作者姓名:刘也  余安喜  朱炬波  唐歌实
作者单位:1.北京航天飞行控制中心航天飞行动力学技术重点实验室, 北京 100094; 2.国防科学技术大学电子科学与工程学院, 长沙 410073; 3.国防科学技术大学理学院, 长沙 410073
基金项目:国家自然科学基金(61072115)
摘    要:指出目标运动先验信息、系统结构信息和设备测量信息的融合应用是提高滤波器跟踪性能的核心。进而综述了弹道目标融合滤波中的运动模型构造、滤波算法设计以及测量误差处理等环节中的关键技术和研究现状。并针对传统实时处理结构弊端,分析了实时跟踪系统的设计方法,讨论了如何建立高效的弹道跟踪数据处理流程,通过融合策略并举的方式实现系统各类信息的有效利用。一些设计方法可以为实际跟踪滤波器的开发提供参考。最后,结合空间应用的发展需求,分析了弹道目标跟踪技术的研究方向。

关 键 词:弹道目标  实时跟踪  滤波  
收稿时间:2012-12-12

Survey of Filter Algorithms for Ballistic Target Real Time Tracking
LIU Ye,YU An xi,ZHU Ju bo,TANG Ge shi.Survey of Filter Algorithms for Ballistic Target Real Time Tracking[J].Journal of Astronautics,2013,34(11):1417-1426.
Authors:LIU Ye  YU An xi  ZHU Ju bo  TANG Ge shi
Affiliation:1.Science and Technology on Aerospace Flight Dynamics Laboratory, Beijing Aerospace Control Center, Beijing 100094, China;   2.College of Electronic Science and Engineering, National University of Defense Technology, Changsha 410073, China;   3.Science College, National University of Defense Technology, Changsha 410073, China
Abstract:The significance for integrated usage of prior dynamic character, system structure and measurement information is suggested. Then, three key steps for the tracking filter are reviewed, i.e. the maneuvering modeling, the nonlinear filter algorithm and the measurement error detection and calibration. Furthermore, designing method for real time tracking system is discussed according to the deficiencies of those existing systems. The method is aim to established an efficiently integrate data processing flow, and achieve an effective fusion of all available system information by hydride fusion strategies. Many actual tracking filter systems can draw lessons from here. Finally, the possible future researches for real time trajectory target tracking are also investigated according to the demand pull space applications.
Keywords:Ballistic target  Real time tracking  Filter  
点击此处可从《宇航学报》浏览原始摘要信息
点击此处可从《宇航学报》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司    京ICP备09084417号-23

京公网安备 11010802026262号