DocumentCode :
3292795
Title :
Sparse Gauss-Hermite Quadrature filter for spacecraft attitude estimation
Author :
Bin Jia ; Ming Xin ; Yang Cheng
Author_Institution :
Mississippi State Univ., Starkville, MS, USA
fYear :
2010
fDate :
June 30 2010-July 2 2010
Firstpage :
2873
Lastpage :
2878
Abstract :
In this paper, a new nonlinear filter based on Sparse Gauss-Hermite Quadrature (SGHQ) is proposed for spacecraft attitude estimation. Gauss-Hermite Quadrature (GHQ) has been widely used in numerical integration and nonlinear filtering. However, for multi-dimensional problems, the conventional GHQ based filter using product operations is difficult to implement because the number of points increases exponentially with dimensions. To solve this problem, the Smolyak´s product rule has been used to extend GHQ rule to high dimensional problems. The contribution of this work is to design a new sparse-grid GHQ filter using Smolyak´s product rule to alleviate the curse-of-dimensionality problem of the conventional GHQ filter. The number of SGHQ points needed for high dimensional problems is considerably smaller than the original GHQ method. Hence, the efficiency of using GHQ can be significantly improved. The performance of this new filter is demonstrated by the application to the spacecraft attitude estimation problem, which shows better results than the Extended Kalman Filter (EKF).
Keywords :
attitude measurement; integration; nonlinear filters; space vehicle electronics; Smolyak product rule; curse-of-dimensionality problem; extended Kalman filter; multidimensional problems; nonlinear filtering; numerical integration; product operations; spacecraft attitude estimation; sparse Gauss-Hermite quadrature filter; Attitude control; Bayesian methods; Filtering; Gaussian noise; Gaussian processes; Multidimensional systems; Noise measurement; Nonlinear equations; Particle filters; Space vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference (ACC), 2010
Conference_Location :
Baltimore, MD
ISSN :
0743-1619
Print_ISBN :
978-1-4244-7426-4
Type :
conf
DOI :
10.1109/ACC.2010.5531487
Filename :
5531487
Link To Document :
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