DocumentCode
174619
Title
Accuracy, efficiency and stability analysis of Sparse-grid Quadrature Kalman Filter in Near space hypersonic vehicles
Author
Hongmei Chen ; Xianghong Cheng ; Chenxi Dai ; Changyan Ran
Author_Institution
Sch. of Instrum. Sci. & Eng., Southeast Univ., Nanjing, China
fYear
2014
fDate
5-8 May 2014
Firstpage
27
Lastpage
36
Abstract
As a recently developed sampling strategy, Sparse-grid quadrature rule has been paid more attention within nonlinear estimation for its high accuracy and low computation cost. Through the Taylor series expansion, the accuracy of Sparse-grid Quadrature Kalman Filter (SGQKF) is analyzed and compared with Quadrature Kalman Filter (QKF). In addition, the computational complexity is analyzed to evaluate the efficiency of SGQKF. The SGQKF asymptotic stability behavior is analyzed by introducing an unknown instrumental diagonal matrix. The theoretical analysis shows that the SGQKF is computationally much more efficient than QKF with the same even higher accuracy; consequently the curse of dimensionality for high dimensional problems can be effectively alleviated. Sufficient conditions for bounded stability are established and it is proved that the estimation error of SGQKF nonlinear systems is exponentially asymptotic. The performance of SGQKF is demonstrated by transfer alignment with large azimuth misalignment angle for Near-space hypersonic vehicle (NSHV), and the simulation results are used to illustrate the benefits of state estimation and modified noise covariance matrix. Our framework is deterministic.
Keywords
Kalman filters; asymptotic stability; autonomous aerial vehicles; computational complexity; covariance matrices; matrix algebra; nonlinear estimation; nonlinear filters; series (mathematics); signal sampling; state estimation; transfer functions; SGQKF nonlinear system; Taylor series expansion; accuracy analysis; azimuth misalignment angle; bounded stability; computational complexity; efficiency analysis; exponential asymptotic stability; instrumental diagonal matrix; near space hypersonic vehicle; noise covariance matrix; nonlinear estimation; sampling strategy; sparse grid quadrature Kalman filter; state estimation; sufficient conditions; transfer alignment; Accuracy; Computational complexity; Covariance matrices; Equations; Noise; Stability analysis; Taylor series; QKF; SGQKF; Taylor expansion; accuracy analysis; computational complexity; near space hypersonic vehicle; stability analysis; transfer alignment;
fLanguage
English
Publisher
ieee
Conference_Titel
Position, Location and Navigation Symposium - PLANS 2014, 2014 IEEE/ION
Conference_Location
Monterey, CA
Print_ISBN
978-1-4799-3319-8
Type
conf
DOI
10.1109/PLANS.2014.6851354
Filename
6851354
Link To Document