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基于样条约束“EMBET”再入轨道测量数据融合方法
引用本文:朱武宣,高耀文.基于样条约束“EMBET”再入轨道测量数据融合方法[J].飞行器测控学报,2005,24(6):49-53.
作者姓名:朱武宣  高耀文
作者单位:北京跟踪与通信技术研究所,北京100094
摘    要:针对再入轨道最小二乘交会解算方法数据利用率低、轨道解算精度差的问题,提出并实现了基于样条约束“EMBET”的再入轨道测量数据融合处理方法.该方法认为再入飞行轨道在时序上是相关的,可以利用三次B样条函数精确表示,建立了关于样条函数参数和测量系统误差的测量模型,从而大量压缩了待估参数数量,准确自校准系统误差,提高了轨道估算的精度和稳定性.

关 键 词:样条函数  再入轨道测量  数据融合  EMBET
收稿时间:2005-07-06
修稿时间:2005-08-22

A Data Fusion Method for Re-entry Ballistic Measurement with Spline Restraint EMBET
ZHU Wu-xuan, GAO Yao-wen.A Data Fusion Method for Re-entry Ballistic Measurement with Spline Restraint EMBET[J].Journal of Spacecraft TT&C Technology,2005,24(6):49-53.
Authors:ZHU Wu-xuan  GAO Yao-wen
Institution:Beijing Institute of Tracking and Telecommunications Technology, Beijing 100094
Abstract:Least square intersection re-entry ballistic calculation method has the disadvantage of inefficient data usage and poor ballistic calculation accuracy. The paper presents and realizes a data fusion method for re-entry ballistic measurement with spline restraint EMBET, The method considers that re-entry ballistic trajectory has great time correlation and can be approached by 3^nd-order B-Spline function. Observation model is established accordingly, System error can be self-calibrated accurately because of reduction of undetermined parameters. As a result, the accuracy and stability of the ballistic calculation are improved.
Keywords:Spline Function  Re-entry Ballistic Measurement  Data Fusion  EMBET
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