Cubature Kalman filtering for orbit determination of space targets

被引：0

作者：

Ning, Xia ^{[1
]}

Ye, Chunmao ^{[2
]}

Yang, Jian ^{[1
]}

Shen, Bin ^{[3
]}

机构：

[1] Department of Electronic Engineering, Tsinghua University, Beijing 100084, China

[2] Beijing Institute of Radio Measurement, Beijing 100854, China

[3] Patent Examination Cooperation Center of the Patent Office, State Intellectual Property Office of P.R.C., Beijing 100088, China

来源：

Dianbo Kexue Xuebao/Chinese Journal of Radio Science | 2014年 / 29卷 / 01期

关键词：

Earth (planet) - Orbits - Kalman filters - Space-based radar;

D O I：

10.13443/j.cjors.2013030101

中图分类号：

学科分类号：

摘要：

For orbit determination of space targets in the low earth orbit, a kind of precise orbit determination method is proposed based on the cubature Kalman filter. Compared with widely used extended Kalman filter, the proposed method provides more accurate state estimation. Moreover, due to the rigorous mathematical proof of the cubature Kalman filter, it achieves good performance on the numerical stability with the complicated motion model during orbit determination. Then, by introducing the sequential posterior Cramér-Rao lower bound, the effect of different radar observation models on the orbit determination performance is analyzed. Finally, using the simulated observation data, the effectiveness of the proposed method and the correctness of the analysis are demonstrated. Copyright © 2014 by Editorial Department of Chinese Journal of Radio Science.

引用

页码：26 / 34

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