计算机应用 ›› 2016, Vol. 36 ›› Issue (5): 1455-1457.DOI: 10.11772/j.issn.1001-9081.2016.05.1455

• 行业与领域应用 • 上一篇    下一篇

基于多项式拟合的扩展卡尔曼滤波算法

吴汉洲1, 宋卫东1, 徐敬青2   

  1. 1. 军械工程学院 火炮工程系, 石家庄 050003;
    2. 军械工程学院 弹药工程系, 石家庄 050003
  • 收稿日期:2015-07-16 修回日期:2015-08-20 出版日期:2016-05-10 发布日期:2016-05-09
  • 通讯作者: 吴汉洲
  • 作者简介:吴汉洲(1989-),男,山东日照人,硕士研究生,主要研究方向:弹箭弹道;宋卫东(1964-),男,河北大名人,教授,博士,主要研究方向:弹道学、弹箭飞行力学;徐敬青(1983-),男,山东青岛人,讲师,博士,主要研究方向:制导弹药。

Extended Kalman filtering algorithm based on polynomial fitting

WU Hanzhou1, SONG Weidong1, XU Jingqing2   

  1. 1. Department of Guns Engeering, Ordnance Engineering College, Shijiazhuang Hebei 050003, China;
    2. Department of Ammunition Engineering, Ordnance Engineering College, Shijiazhuang Hebei 050003, China
  • Received:2015-07-16 Revised:2015-08-20 Online:2016-05-10 Published:2016-05-09

摘要: 弹道修正弹内的弹载计算机必须实时对卫星定位接收机获取的弹丸状态数据进行滤波降噪,用于预测弹丸落点,传统滤波方法滤波时间长,滤波实时性差,提出一种基于多项式拟合的方法。通过适当降低卫星定位接收机数据更新频率,并用多项式拟合插值出的数据代替数据更新时间间隔内的弹丸状态数据。仿真实验表明,该算法在不降低滤波效果的前提下,较普通扩展卡尔曼滤波时间降低7/8,提高了滤波实时性,对于弹道修正弹关键技术的研究提供了重要参考。同时该方法可推广应用到其他滤波算法当中,具有很强的可移植性。

关键词: 滤波算法, 多项式拟合, 弹道修正弹, 卫星定位数据, 滤波误差

Abstract: The data acquired by the satellite positioning receiver in the trajectory correction projectile must be filtered in real-time to predict the point. The calculation of traditional filtering method is time-consuming, and is difficult to meet the requirements of real-time filtering. A kind of extended Kalman filtering algorithm based on polynomial fitting was proposed. The data of projectile flight in the time interval was replaced by the fitting interpolation data. In this way the filter frequency could be reduced. Simulation results show that the computation time of the proposed method can be reduced by 7/8 compared to traditional extended Kalman filtering without reducing the filtering precision, and the real-time performance is improved. This method can provide important reference for the research of key technology of trajectory correction projectile. At the same time, the method can be applied to other filtering algorithms, and has a strong portability.

Key words: filtering algorithm, polynomial fitting, trajectory correction projectile, satellite positioning data, filtering error

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