UPF based autonomous navigation scheme for deep space probe

被引：7
|
作者：
Li Peng [1 ]
Cui Hutao [1 ]
Cui Pingyuan [1 ]
机构：
[1] Harbin Inst Technol, Deep Space Explorat Res Ctr, Harbin 150080, Peoples R China
来源：
JOURNAL OF SYSTEMS ENGINEERING AND ELECTRONICS | 2008年 / 19卷 / 03期
关键词：
control and navigation technology of aircraft; nonlinear and non-Gaussian; unscented particle filter; autonomous orbit determination; celestial navigation; optical navigation;
D O I：
10.1016/S1004-4132(08)60117-6
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
The autonomous "celestial navigation scheme" for deep space probe departing from the earth and the autonomous "optical navigation scheme" for encountering object celestial body are presented. Then, aiming at the conditions that large initial estimation errors and non-Gaussian distribution of state or measurement errors may exist in orbit determination process of the two phases, UPF (unscented particle filter) is introduced into the navigation schemes. By tackling nonlinear and non-Gaussian problems, UPF overcomes the accuracy influence brought by the traditional EKF (extended Kalman filter), UKF (unscented Kalman filter), and PF (particle filter) schemes in approximate treatment to nonlinear and non-Gaussian state model and measurement model. The numerical simulations demonstrate the feasibility and higher accuracy of the UPF navigation scheme.
引用
收藏
页码：529 / 536
页数：8
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