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CLC number: TP2; V52

On-line Access: 2013-06-04

Received: 2012-10-15

Revision Accepted: 2013-05-04

Crosschecked: 2013-05-13

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Journal of Zhejiang University SCIENCE C 2013 Vol.14 No.6 P.425-432


Feasibility analysis for attitude estimation based on pulsar polarization measurement

Author(s):  Nan Luo, Lu-ping Xu, Hua Zhang, Qiang Xie

Affiliation(s):  School of Electronic Engineering, Xidian University, Xi’an 710071, China

Corresponding email(s):   nluo@mail.xidian.edu.cn

Key Words:  Pulsar, Polarization, Attitude determination, Stable factor

Nan Luo, Lu-ping Xu, Hua Zhang, Qiang Xie. Feasibility analysis for attitude estimation based on pulsar polarization measurement[J]. Journal of Zhejiang University Science C, 2013, 14(6): 425-432.

@article{title="Feasibility analysis for attitude estimation based on pulsar polarization measurement",
author="Nan Luo, Lu-ping Xu, Hua Zhang, Qiang Xie",
journal="Journal of Zhejiang University Science C",
publisher="Zhejiang University Press & Springer",

%0 Journal Article
%T Feasibility analysis for attitude estimation based on pulsar polarization measurement
%A Nan Luo
%A Lu-ping Xu
%A Hua Zhang
%A Qiang Xie
%J Journal of Zhejiang University SCIENCE C
%V 14
%N 6
%P 425-432
%@ 1869-1951
%D 2013
%I Zhejiang University Press & Springer
%DOI 10.1631/jzus.C1200291

T1 - Feasibility analysis for attitude estimation based on pulsar polarization measurement
A1 - Nan Luo
A1 - Lu-ping Xu
A1 - Hua Zhang
A1 - Qiang Xie
J0 - Journal of Zhejiang University Science C
VL - 14
IS - 6
SP - 425
EP - 432
%@ 1869-1951
Y1 - 2013
PB - Zhejiang University Press & Springer
ER -
DOI - 10.1631/jzus.C1200291

One of the important characteristics of pulsar radiation is polarization. It is considered not only as a probe for recognizing the structure of a magnetic field, but also as a lighthouse for estimating spacecraft attitude via orientation information between the pulsar and the detector. Although polarization of a pulsar has been studied for decades, until recently applications to determination of spacecraft attitude have been seldom reported. This paper deals with analysis of the feasibility of applying polarization information to attitude estimation. The stability factor (SFR) and observation fluctuation factor (OFR) are introduced to analyze the stability of a pulsar’s polarized position angle. Based on European pulsar Network (EPN) data, several simulated instances are used to demonstrate that the accuracy requirement of attitude determination can be met via polarization measurement. The SFR of a pulsar is evaluated using simulated polarization data, and the OFR is used to analyze the relationship between fluctuation extent and observation time. Simulation results show that the polarized measurement of candidate pulsars PSR B0470-28 and PSR B2319+60 reaches the specification for attitude determination.

Darkslateblue:Affiliate; Royal Blue:Author; Turquoise:Article


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