A New Non-singular Terminal Sliding Mode Guidance Law for Surface-to-Air Missile

CUI Xi; DAI Juan; FAN Cunli; SU Zhong; LIU Hong; ZHU Cui

doi:10.3969/j.issn.1671-637x.2021.01.009

Journals >Electronics Optics & Control >Volume 28 >Issue 1 >Page 37 > Article

Electronics Optics & Control
Vol. 28, Issue 1, 37 (2021)

A New Non-singular Terminal Sliding Mode Guidance Law for Surface-to-Air Missile

CUI Xi^1、2、3, DAI Juan^1、2、3, FAN Cunli^1、2、3, SU Zhong^1、2、3, LIU Hong^1、2、3, and ZHU Cui⁴

Author Affiliations

¹[in Chinese]

²[in Chinese]

³[in Chinese]

⁴[in Chinese]

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DOI: 10.3969/j.issn.1671-637x.2021.01.009 Cite this Article

CUI Xi, DAI Juan, FAN Cunli, SU Zhong, LIU Hong, ZHU Cui. A New Non-singular Terminal Sliding Mode Guidance Law for Surface-to-Air Missile[J]. Electronics Optics & Control, 2021, 28(1): 37 Copy Citation Text

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References

[3] BHAT S P, BERNSTEIN D S.Continuous finite-time stabilization of the translational and rotational double integrators［J］.IEEE Transactions on Automatic Control, 1998,43(5):678-682.

[6] KUMAR S R, RAO S, GHOSE D.Sliding-mode guidance and control for all-aspect interceptors with terminal angle constraints［J］.Journal of Guidance, Control, and Dynamics, 2012, 35(4):1230-1246.

[9] ZHU Z, XIA Y Q, FU M Y.An observer-based missile guidance law［C］//Chinese Control and Decision Conference (CCDC), 2011:1282-1287.

CUI Xi, DAI Juan, FAN Cunli, SU Zhong, LIU Hong, ZHU Cui. A New Non-singular Terminal Sliding Mode Guidance Law for Surface-to-Air Missile[J]. Electronics Optics & Control, 2021, 28(1): 37

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