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基于测速定轨的一类自适应样条滤波方法
引用本文:周海银,汪雄良,朱炬波. 基于测速定轨的一类自适应样条滤波方法[J]. 国防科技大学学报, 2001, 23(6): 38-41
作者姓名:周海银  汪雄良  朱炬波
作者单位:国防科技大学理学院,
基金项目:国家自然科学基金 ( 6 9872 0 39),教育部振兴计划高校骨干教师资助计划项目
摘    要:提出了一种测速定轨的实时算法。该方法基于样条表示飞行轨道速度参数 ,在只有多个测速元信息的情况下 ,建立了自适应Kalman滤波递推算法 ,实时给出了较高精度的飞行器轨道参数

关 键 词:测速定轨  自适应  样条滤波
文章编号:1001-2486(2001)06-0038-04
收稿时间:2001-05-09
修稿时间:2001-05-09

Self-adaptive Spline Filter Approach for Trajectory Determination by Velocity Measurement
ZHOU Haiyin,WANG Xiongliang and ZHU Jubo. Self-adaptive Spline Filter Approach for Trajectory Determination by Velocity Measurement[J]. Journal of National University of Defense Technology, 2001, 23(6): 38-41
Authors:ZHOU Haiyin  WANG Xiongliang  ZHU Jubo
Affiliation:College of Science, National Univ. of Defense Technology, Changsha 410073,China;College of Science, National Univ. of Defense Technology, Changsha 410073,China;College of Science, National Univ. of Defense Technology, Changsha 410073,China
Abstract:Based on spline filtering, this paper presents a novel self-adaptive approach for trajectory determination by using velocity measurements. The spline function is adopted to express the parameters of the trajectory so that an iterative algorithm of self-adaptive Kalman filter is established. When information of velocity measurement is merely provided, this approach can give real-time trajectory parameters of the aircraft with high precision .
Keywords:self adaptive  spline filter  trajectory determination by velocity measurement
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