Recursive Range Estimation Using Astrophysical Signals of Opportunity

被引:6
|
作者
Runnels, Joel T. [1 ]
Gebre-Egziabher, Demoz [1 ]
机构
[1] Univ Minnesota, Aerosp Engn & Mech Dept, 110 Union St SE, Minneapolis, MN 55455 USA
关键词
DELAY FIR FILTERS; SPACECRAFT NAVIGATION; TIME-DELAY; PULSAR; MILLISECOND; TELESCOPE; DESIGN; RAYS;
D O I
10.2514/1.G002650
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
An estimator for determining the range of a space vehicle relative to some origin by using astrophysical signals of opportunity is developed. The signals used are x-ray photons emitted by pulsars. The estimator is an extended Kalman filter, which estimates the time difference of arrival of x-ray photons at the space vehicle and the origin. The performance of the estimator is validated by Monte Carlo simulations and postprocessing x-ray data from the NASA/Japan Aerospace Exploration Agency Suzaku mission. It is found that the proposed algorithm performance is comparable (as measured by estimation error covariance) to the maximum-likelihood estimator used on this problem, which has been successfully used on a similar x-ray pulsar navigation problem in the past.
引用
收藏
页码:2201 / 2213
页数:13
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