Finite-Time Convergent Sliding Mode Guidance Law with Impact Angle Constraint

ZHANG Kai; YANG Suo-chang; ZHANG Kuan-qiao; YAO Yun-zhi; CHEN Peng

doi:10.3969/j.issn.1671-637x.2017.01.015

Journals >Electronics Optics & Control >Volume 24 >Issue 1 >Page 63 > Article

Electronics Optics & Control
Vol. 24, Issue 1, 63 (2017)

Finite-Time Convergent Sliding Mode Guidance Law with Impact Angle Constraint

ZHANG Kai¹, YANG Suo-chang¹, ZHANG Kuan-qiao¹, YAO Yun-zhi¹, and CHEN Peng²

Author Affiliations

¹[in Chinese]

²[in Chinese]

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DOI: 10.3969/j.issn.1671-637x.2017.01.015 Cite this Article

ZHANG Kai, YANG Suo-chang, ZHANG Kuan-qiao, YAO Yun-zhi, CHEN Peng. Finite-Time Convergent Sliding Mode Guidance Law with Impact Angle Constraint[J]. Electronics Optics & Control, 2017, 24(1): 63 Copy Citation Text

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References

[1] KIM M, GRIDER K V.Terminal guidance for impact attitude angle constrained flight trajectories［J］.IEEE Tran-sactions on Aerospace and Electronic Systems, 1973, 9(6):852-859.

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ZHANG Kai, YANG Suo-chang, ZHANG Kuan-qiao, YAO Yun-zhi, CHEN Peng. Finite-Time Convergent Sliding Mode Guidance Law with Impact Angle Constraint[J]. Electronics Optics & Control, 2017, 24(1): 63

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