Interacting Multiple Mode Tracking Algorithm Based on Modified Coordinate Turn Model

Article Preview

Abstract:

The continuing success of near space hypersonic aircraft flight test has become a real threat to China's space attack-defense system, In view of the problem that the single model cannot track such target effectively, an interacting multiple model (IMM) tracking algorithm based on modified cornering model (MCT) was proposed. First the characteristics of near space hypersonic target were analyzed, and then the target real-time angular velocity according to the target motion equation was estimated, finally the near space hypersonic target tracking through the IMM was carried out. The Monte Carlo simulation results show that the IMM tracking algorithm can effectively track near space hypersonic target, and the tracking accuracy and stability are superior to single model, it has certain practical significance.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

534-539

Citation:

Online since:

August 2014

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2014 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] R F Hu, Z N Wu, Z Wu. Aerodynamic map for soft and hard hypersonic level flight in near space, Acta Mech Sin. 2009, 25(4): 571-575.

DOI: 10.1007/s10409-009-0264-4

Google Scholar

[2] W A DING. Singel-station location and tracking methods on direction and frequency measurement combined with improved least-squares algorithm, Journal of Detection & Control. 2011, 3(1): 61-64.

Google Scholar

[3] X GUAN, J ZHAO, HE Y. Track technology of hypersonic aircraft in near space, Journal of Sichuan Ordnance. 2011, 32(8): 4-6.

Google Scholar

[4] X GUAN, J ZHAO, Z C ZHANG. A feasible tracking algorithm for hypersonic aircraft, Telecommunication Engineering. 2011, 51(8): 80-84.

Google Scholar

[5] E. Mazor, A. Averbuch, S Y Bar. Interacting multiple model methods in target tracking: a survey, IEEE Trans. On Aerospace and Electronic Systems. 1998, 34(1): 103-123.

DOI: 10.1109/7.640267

Google Scholar

[6] C. Graham, H. Johnson, C. Alba. Analysis of modal growth on the leeward centerplane of the X-51 vehicle, USA: University of Minnesota (2009).

DOI: 10.21236/ada513296

Google Scholar

[7] Robinson, S. Jeffrey. An overview of NASA's integrated design and engineering analysis (IDEA) environment, USA: American Institute of Aeronautics and Astronautics (2011).

Google Scholar