Finite-Time Hovering Control of Unmanned Helicopter Based on Sliding Mode Method

ZHANG Miao; MA Jianwei; GAO Jiwei; ZANG Shaofei

doi:10.3969/j.issn.1671-637x.2023.08.008

Journals >Electronics Optics & Control >Volume 30 >Issue 8 >Page 43 > Article

Electronics Optics & Control
Vol. 30, Issue 8, 43 (2023)

Finite-Time Hovering Control of Unmanned Helicopter Based on Sliding Mode Method

ZHANG Miao, MA Jianwei, GAO Jiwei, and ZANG Shaofei

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[in Chinese]

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DOI: 10.3969/j.issn.1671-637x.2023.08.008 Cite this Article

ZHANG Miao, MA Jianwei, GAO Jiwei, ZANG Shaofei. Finite-Time Hovering Control of Unmanned Helicopter Based on Sliding Mode Method[J]. Electronics Optics & Control, 2023, 30(8): 43 Copy Citation Text

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References

[4] TAYEBI A.Unit quaternion-based output feedback for the attitude tracking problem［J］.IEEE Transactions on Automatic Control,2008,53(6):1516-1520.

[11] DEFOORT M,FLOQUET T,KOKOSY A M,et al.A novel higher order sliding mode control scheme［J］.Systems and Control Letters,2008,58(2):102-108.

ZHANG Miao, MA Jianwei, GAO Jiwei, ZANG Shaofei. Finite-Time Hovering Control of Unmanned Helicopter Based on Sliding Mode Method[J]. Electronics Optics & Control, 2023, 30(8): 43

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