Active Fault Tolerant Control of Aircraft Based on Integral Sliding Mode Control

LI Li-rong; LIU Chun-sheng

doi:10.3969/j.issn.1671-637x.2019.03.004

Journals >Electronics Optics & Control >Volume 26 >Issue 3 >Page 16 > Article

Electronics Optics & Control
Vol. 26, Issue 3, 16 (2019)

Active Fault Tolerant Control of Aircraft Based on Integral Sliding Mode Control

LI Li-rong and LIU Chun-sheng

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[in Chinese]

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DOI: 10.3969/j.issn.1671-637x.2019.03.004 Cite this Article

LI Li-rong, LIU Chun-sheng. Active Fault Tolerant Control of Aircraft Based on Integral Sliding Mode Control[J]. Electronics Optics & Control, 2019, 26(3): 16 Copy Citation Text

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References

[4] SIDIM J.Spacecraft dynamics and control:a practical engineering approach［M］.Cambridge:Cambridge University Press, 1997.

[8] XU J X, PAN Y J, LEE T H.Analysis and design of integral sliding mode control based on Lyapunov′s direct method［C］//American Control Conference, Denver, 2003:192-196.

LI Li-rong, LIU Chun-sheng. Active Fault Tolerant Control of Aircraft Based on Integral Sliding Mode Control[J]. Electronics Optics & Control, 2019, 26(3): 16

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