Design of 3-Dimensional Guidance Law of Missile Based on Discrete Sliding Mode

Nuan Wen; Zheng Hua Liu; Le Chang

doi:10.4028/www.scientific.net/AMR.816-817.976

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 816-817Design of 3-Dimensional Guidance Law of Missile...

Design of 3-Dimensional Guidance Law of Missile Based on Discrete Sliding Mode

Abstract:

In this article, a new approach to design discrete-time sliding-mode guidance laws is presented based on the target-missile relative motion equation in three-dimensional space. This method significantly reduced system chattering and could be easily achieved on engineering. Furthermore, effectiveness of the proposed guidance laws is demonstrated through simulation by comparing with the traditional proportional guidance laws.

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Periodical:

Advanced Materials Research (Volumes 816-817)

Pages:

976-980

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.816-817.976

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Online since:

September 2013

Authors:

Nuan Wen, Zheng Hua Liu, Le Chang

Keywords:

3-Dimensional Space, Discrete Time, Guidance Laws, Variable Structure

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References

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