An Estimation Approach Based on Predictive Filtering to Missile Guidance

Yuan Yun Song; Wan Chun Chen; Xing Liang Yin

doi:10.4028/www.scientific.net/AMR.383-390.38

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 383-390An Estimation Approach Based on Predictive...

An Estimation Approach Based on Predictive Filtering to Missile Guidance

Abstract:

An approach for estimation to states of missile guidance based on predictive filtering is derived for the measurement process with high and low frequency noise. Analyze the influence of various noises on miss distance. Comparing with the extended Kalman filter, the simulation results indicate that this new method is able to improve accuracy of the guidance system with less estimation error.

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Manufacturing Science and Technology, ICMST2011

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Periodical:

Advanced Materials Research (Volumes 383-390)

Pages:

38-44

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.383-390.38

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Online since:

November 2011

Authors:

Yuan Yun Song, Wan Chun Chen, Xing Liang Yin

Keywords:

Filter, Guidance, Kalman Filter (KF), Missile, Predictive Filtering

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References

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