Carrier Aircraft Urgent Takeoff In-Flight Alignment Extended Set-Membership Estimation

Article Preview

Abstract:

This paper considers the nolinear system robust estimation problem with measurement time delay. The purpose is to provide algorithm for inertial navigation system nonlinear error model in transmittion delay case. Considering that innovation regroup method can treat the measurement delay problem better with no addition of system state dimension, and decrease the system computation, therefore, that algorithm is combined with extended set-membership estimation and deduce the distrete nonlinear system extended set-membership estimation algorithm with measurement delay, realize nonlinear system varying state estimation and the treatment of measurement delay. At last, apply the algorithm to carrier aircraft in-flight alignment and validate the effecitiveness.

You might also be interested in these eBooks

Info:

Periodical:

Advanced Materials Research (Volumes 945-949)

Pages:

2772-2779

Citation:

Online since:

June 2014

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2014 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] Sun Xianfang, Wang Shiji, Zhang Hai. The application of extended set-membership filtering in the strap-down inertial navigation system large azimuth misalignment initial alignment[J]. Journal of Chinese inertial technology, 2008, 16(5): 505-508.

Google Scholar

[2] Scholte E, Campbell M. A nonlinear set-membership filters for on-line applications[J]. International Journal of Robust Nonlinear Control, 2003, 13(15): 1337-1358.

DOI: 10.1002/rnc.856

Google Scholar

[3] Zhao Hongguo, stable robust optimal control and filter of input-output time delay system[D]. Shandong university, (2008).

Google Scholar

[4] Lu Xiao, optimal filtering of observation time delay system[D]. Dalian science university, (2008).

Google Scholar

[5] Zhang H S, Xie L H, Zhang D, et a1.A reorganized innovation approach to linear estimation[J]. IEEE Transactions on Automatic Control, 2004, 49(10): 1810-1814.

DOI: 10.1109/tac.2004.835599

Google Scholar

[6] Dai Hongde. Research on carrier aircraft inertial navigation system moving base alignment technology [D]. Northwest industrial university, (2008).

Google Scholar

[7] Cao Juanjuan, Fang Jiancheng, Sheng Wei. MIMU in-flight alignment model and semi-physics simulation of large azimuth misalignment[J]. Journal of Beijing aeronautical and astronautical university, 2008, 34(11): 63-66.

Google Scholar

[8] Gao Chao. Research on multi-source assistant alignment and information source evaluation technology of carrier aircraft [D]. Naval aeronautical engineering academy, (2010).

Google Scholar